On-line: гостей 0. Всего: 0 [подробнее..]
Добро пожаловать!
Форум ВКО открыт для дискуссий.



АвторСообщение



Сообщение: 2
Зарегистрирован: 29.08.10
Репутация: 0
ссылка на сообщение  Отправлено: 29.08.10 22:57. Заголовок: подавление GPS приемников


Добрый вечер.
Есть ли возможность получить компетентный ответ (хотя бы в общем) от специалиста в области РЭБ?
Собственно интересует, возможно ли на нынешнем этапе эффективное подавление военных GPS приемников? С одной стороны подобные разработки есть и рекламируются, но "спецы" работающие с GPS говорят, что заявленные для таких систем дальность подавления в 100-150 км реальны только для гражданских изделий и для военных приемников эти значения будут составлять не более 150-200 метров. То есть, по факту, против ВТО с системами спутниковой коррекцией не эффективны.

Спасибо: 0 
ПрофильЦитата Ответить
Новых ответов нет , стр: 1 2 3 4 All [см. все]


moderator




Сообщение: 4083
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 29.08.10 23:36. Заголовок: Есть ли возможность ..


Есть ли возможность получить компетентный ответ (хотя бы в общем) от специалиста в области РЭБ?

1. ne jawljaus' takim

2. Собственно интересует, возможно ли на нынешнем этапе эффективное подавление военных GPS приемников?

Mozno ...

a. 1575.42MHz (GPS) . Woennij priemnik DAGR

http://en.wikipedia.org/wiki/Defense_Advanced_GPS_Receiver<\/u><\/a>

Naibolee ystojchiwaja sistema k pomexam Milstar/AEHF
ona 20/44ghz

USA ne daet 100 % garantii

Chem wische diapazon ,tem wische koef. naprawlennosti antenni

shirina lucha antenni diametrom 1.8 metra na 20 ghz - 0.5 grad
############################################

na snimke DAGR mozet srawnit' welichinu antenni DAGR s antennoj diamtrom 1.8 metra
Ychtite chto dlja odnoj i toj ze antenni 1.8 metra ,odna na GPS band -1575 mgz ,drugaja na 20 ghz podawit' 1575 mgz gorazdo prosche , w slsuchae priemnika
DAGR tem bolee -antenni dimatrom 1.8 metra net


То есть, по факту, против ВТО с системами спутниковой коррекцией не эффективны.

Esli wozmozno sdelat* pomexu protiw milstar/AEHF w diapazone 44/20 GHZ
s boslchimi antennami i antennami nulifikatorami ,to protiv GPS prosche ...


1. Awtonomnie sistemi -AIRS /inerzionalnij datchik MX
daet tochnost' 1 metr na 10 000 km / tochnost' rulewogo yprawlenija w 50-90 raz xuze/

Podawit' - prjamim popadaniem w golowku s Yabch

2. Astrokorrekzija - ne yawljaetsja polnostju awtonomnoj ,no mozet redko na kaom -to ychastke traektorii w korotkoe wremja wwodit' korrekziju po zwezdam


3. GPS - ne awtonomnaja ,ni w odnoj ballisticheskoj rakete bez nalichija perwix dwux
*************************************************************************
ne ispolzuetsja
*************

что заявленные для таких систем дальность подавления в 100-150 км реальны только для гражданских изделий и для военных приемников эти значения будут составлять не более 150-200 метров

? ochen bolschoe razlichie -maloverojatno dlja woennix i grazdanskix priemnikow
#######################################################
primerno rawnogo klassa po stoimsoti
##########################

1.sootnoschenie signal/schum y woennix mozet bit' poluchsche ,no kriogennowogo oxlazdenija ne wizu ...

2. Ky. antenni i moschnost' istochnika pomexi , naxozdenie priemnika kotorij dolzen bit' podawlen ,sputnikow i istochnika/istochnikow pomexi

3 .Podriw yabch,neskolkix yabch podawit proxozdenie signala GPS
( wisokaja ionizacija atmosferi trebuet antenn 40 kw .metrow w diapazone
35 ghz i msochnostej po 1 megawatu)


http://www.prc68.com/I/DAGR.shtml<\/u><\/a>









Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4085
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 29.08.10 23:56. Заголовок: http://www.fas.org/s..


http://www.fas.org/spp/military/program/nav/labjam.pdf<\/u><\/a>


GPS Jamming in A Laboratory Environment
Gregory D. Rash
Naval Air Warfare Center Weapons Division (NAWCWPNS)/China Lake


The author would like to thank Mr. Daniel Crabtree and
Mr. Sherryl Stovall of the Navigation and Data Link
Section for their assistance and guidance in preparing this
paper. Special thanks to Mr. David Ferrucci and Mr. Bo
Shaw of the F/A-18 Weapons System Support Activity for
their sponsorship of this work.


This paper has presented the major issues and problems
associated with generating GPS jamming. The
importance of maintaining QC was discussed, and a brief
example was given detailing one approach to designing
and fabricating a GPS jamming system suitable for
laboratory use.

about author

Greg Rash received his Bachelor of Science in Electrical
Engineering from Fresno State University in 1991.
Employed by the Naval Air Warfare Center Weapons
Division (NAWCWPNS), China Lake, California, he has
worked on the development of phased-array antennas and
has performed simulation, analysis, modeling, and testing
for various missile programs. His first exposure to the
Global Positioning System (GPS) occurred when he was
------------------------------------------------------------------
tasked as the GPS system engineer for Tomahawk Cruise
---------------------------------------------------------------------
Missile in mid 1993.
--------------------------
In late 1995 he started developing a
remotely controllable GPS jamming system for laboratory
use. Greg is currently part of the design team tasked with
integrating an EGI for use in a real-time simulation
application at the NAWCWPNS Navigation Laboratory.

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4086
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 30.08.10 00:05. Заголовок: BAE Systems develops..


BAE Systems develops anti-jamming GPS receivers


AUSTIN, Texas, 18 April 2008. BAE Systems has developed a satellite navigation receiver system designed to provide uninterrupted operation of the global positioning system for air, land, and sea platforms and applications.

The company developed and readied the system in response to the emerging threat of disruption to operations of GPS navigation systems. The new satellite navigational immune receiver ensures operable navigation in the presence of radio-requency jamming.

"GPS jamming has become an acute threat to armed forces operating in the modern battle arena," says Kent Jacobson, vice president of BAE Systems' Sensor Integration business in Austin. "BAE Systems developed a unique system that offers operational immunity against electronic jamming and disruptions to maintain precise and reliable GPS operation, even in multiple jamming environments."

During tests of the system, the anti-jam GPS overcame electronic jamming in various scenarios, including multiple simultaneous jamming.
------------------------------------------------

Zawisit ot scenarija - w ljubom sluschae jamming bolee nizkogo diapazona 1.524 ghz
dlja GPS s nenapr. antennoj

gorazdo prosche chem 44/20 ghz Milstar/AEHF s wiskonapr. antennami po 1.8 metra


Poslednee wozmozno ,xotja tjazelo (po ytwerzd. razr .Milstar/AEHF)

Milstar/AEHF po istochniku pitanija pomoschnee 10-15 kwt ,no podalsche 37 000 km
protiw 20 000 y GPS

http://www.militaryaerospace.com/index/display/article-display/326201/articles/military-aerospace-electronics/online-news-2/2008/04/bae-systems-develops-anti-jamming-gps-receivers.html<\/u><\/a>

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4087
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 30.08.10 00:07. Заголовок: http://www.fas.org/s..

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4091
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 30.08.10 00:47. Заголовок: Radar performance de..


Radar performance degrades in environments disturbed by nuclear explosions.
###################################################
Hit- to-kill GBIs eliminate the nuclear weapon in the interceptor, but not that in the incoming RV, which could detonate on contact or command.
#######################################

Neskolko yglow attaki ,na kazdom formazija/gruppirowka po 100 -1000 boegolowok

W ochen' xoroschim/xoroschim chansom chast' iz nix budet podorwanna
po prodwizeniju k rajonu attaki dlja degradazii/polnoj newozmoznosti
funkzionirowanija rls PRO/BMD

That would produce widespread ionospheric disturbances that could interrupt radar or infrared sensors for times longer than the attack.
#################################
The US has no relevant data on nuclear phenomenology at relevant intercept altitudes.
#######################################################
While x-band radars are less susceptible to nuclear blackout, the Achilles heel of Sentinel and Safeguard was random refraction from multiple bursts, for which there is no experimental evidence.
#####################

Wopros s 35 ghz i 94 ghz RLS ,budut oni lutsche w dannoj situazii ?

s ychetom wozmoznix plusow - ochen' yzkij luch ,dlja cassegran antenni 13.7 metra diametorom 0.014 grad dlja 94 ghz i 0.042 grad dlja 35 ghz
i minusow - pri nizkix yglax bolschoe zatuxanie ot atmosferi ,w dozd' rsche xuze
Megawatnnie lampi est' na oba diapazona

pri depressed traektori wisota poleta mozet bit' 50-60 km
pri elevazii 0 grad eto 800 km
Y Warlok pri antenne 1.8 metra 94 ghz i impulsnoj moschnosti 100 kwt
pri yglax elevazii 30 grad- 700 km
pri 0 grad -70 km

W 7 raz bolsche antenna = 49 po moschnosti i 10 po moschnsoti
= 490.Koren' chetwertoj stepeni daet ywelichenie dalnosti
w 4.7 raza

Na 35 ghz werojatno lutsche(zatuxanie w atmosfere i ot dozdja mensche ) ,
no za schet ywelichanija lucha s 0.014 grad w 0.042 grad

For attacks greater than a few weapons, this introduces a fundamental uncertainty into
########################################################
NMD.
###

Gregory H. Canavan

Los Alamos National Laboratory

gcanavan@lanl.gov

http://www.aps.org/units/fps/newsletters/1999/july/canavan-paper.html<\/u><\/a>


Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4232
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 09.09.10 14:05. Заголовок: Draper laboratory ..


Draper laboratory - stat*ja o pomexaxwoennim GPS priemnikam

http://www.draper.com/digest97/paper5.pdf<\/u><\/a>

Nominal GPS level L2 -166dbw

smotri grafik 8

signal GPS s moschnsot*ju 10 w -16 mozet bit* ispolzowan pri nalichii moschnsoti pomex 10 w -12

t.e. 40 db raznici .mozno sdelat* boslche chem 40 db bez problem


Ogranichennost* GPS

1. Rasstojanie 20 000 km protiw istochnika pomexi w 100 raz blize = 200 km

snizenie rasstojanija w 2 raza = ywelicheniju moschnosti w 4 raza

w 100 raz -w 10 000 raz

2. Antenna peredatchika i priemnika ne naprawlena i chastota dowlno newisokaja 1.5 ghz


3. Moschnost* peredatchika sputnika ( moschnsot* battarej do 10 kwt w lutschem sluchae)

4. Moschnost* peredatchika pomexi mozno bez problem sdelat * 100 kilowatt -1 megawatt (na chassi
YAZ-Tigr-Kamaz - z/D Vagon) .Antennu naprawlennoj

1.8 metra 1.5 ghz eto 6.5 grad schirina lepestka

*************************************************

ykazanna wozmoznsot* raboti woennogo priemnika pri signale pomexi na 40 db prew. poleznij signal

na grafike na ris 8 pri signale pomexi 10 kwt i nenaprawlennoj antenne

signal pomexi na 70 db bolsche na rasstojanii 100 mil (160 km)
**********************************************************

100 kwt -budet na 80 db (limit raboti woen. priemnika 40 db)
1 megawatt -budet na 90 db

+ Ky naprawlennoj antenni

pri diametr 4.8 metra gain dlja 1.6 ghz budet primerno 36- 37 db
****************************************************

http://www.gdsatcom.com/Antennas/Data_Sheets/6550034D_4.8m.pdf<\/u><\/a> (ykazan dlja 3.6 ghz -44 db ,dlja 1.6 ghz
otnjat 7-8 db)

Itogo pri 100 kwt 117 db na 160 km ( limit woennogo priemnika 40 db)
***************************************************************

Poetomu novie razrabotki GPS sputnika rassmatriwajut wozmoznost* ispolzowanija naprawlennix antenn

Mozno ispolzowat* i w priemnike ,no gabrati priemnika GPS ogranicheni gabaritami raketi (Tomogawk )

lampi megawatnogo klassa na 1.6 ghz w SSSR est* w masse s 50 godow


*************************
Lans wrote -

29.08.10 23:57. Заголовок: подавление GPS приемников

Добрый вечер.
Есть ли возможность получить компетентный ответ (хотя бы в общем) от специалиста в области РЭБ?

... detali mozete sprosit* yawtora stat*i


jlozow@draper.com
***************************************


o Draper laboratory

Modernizing the Nation’s Strategic Missile Guidance Systems
*************************************************
Draper is applying its guidance, navigation, and control (GN&C) expertise to maintain and modernize Navy and Air Force strategic missile guidance capabilities.

Technology: Developing Inertial Instrument Technology for Strategic Applications
To help the Navy’s Strategic Guidance Program achieve higher reliability and lower life-cycle maintenance costs through MK6 Life Extension (MK6LE) efforts, Draper has been developing new designs for critical sensors. The new Alternate Pendulous Integrating Gyroscopic Assembly (Alt-PIGA) and the all-solid-state Interferometric Fiber-Optic Gyroscope (IFOG) will replace older electromechanical, spinning mass devices that have many small, precision parts in a complex assembly. The new charge coupled device (CCD) to be used in the MK6LE stellar camera is a 128 x 128 array being developed in conjunction with e2v Corporation.

Draper’s Silicon Oscillating Accelerometer (SOA) design has progressed in support of the Air Force Research Laboratory and the Navy’s objective of advancing strategic-grade accelerometer technologies. A circumvention and recovery scheme that allows the OA toS recover rapidly following pulse radiation exposure has been demonstrated.

Execution: MK6LE
As the Prime Contractor for the Navy’s Trident D5 missile guidance system, Draper Laboratory oversees the MK6LE
************************************************************************************************
development team of more than 700 engineers from Draper and its major subcontractors as it modernizes the missile’s MK6 inertial guidance system. The goal is to extend the MK6 guidance system life to 2042 while lowering the
*************************************************************************************************

Navy’s future maintenance and support costs and provide a flexible architecture to support new missions and upgrades. Draper continues to maintain the MK6 guidance system currently deployed in the Trident submarine fleet.

Critical to MK6LE program success is affordability and technical risk reduction. Draper is employing sophisticated modeling and simulation techniques to verify designs well in advance of fabricating production hardware. These models are also integrated into a virtual guidance system to provide stimulus to subsystem prototypes to verify their designs.

Execution: Maintain Minuteman III to 2030 and Beyond
*********************************************

As the original Design Agent for the Minuteman III PIGA accelerometer, Draper provides support to Northrop Grumman Mission Systems, the Prime Integrating Contractor for the Air Force. Draper performs accuracy and reliability analyses and addresses the problem of parts obsolescence by qualifying new vendors, parts, and processes, and supports the repair of the Minuteman III PIGA.

Simulation: Enhanced Ground Test (EGT)
Draper conceptualized and designed the Enhanced Ground Test (EGT), which simulates missile environments through a series of nondestructive tests. EGT will be able to assess MK6LE guidance system performance with its new inertial instruments incorporated. This major innovation holds the potential to augment guidance flight tests for accuracy and reliability evaluations as well as to mitigate MK6LE development risk. It will analyze and integrate test data measured during a series of simulated flight tests executed using a precision centrifuge, an aircraft guidance system pod flown on an F-15E, and shock and vibration tests. Test and analysis results (accuracy and reliability) have shown a high correlation to flight performance, verifying the initial EGT approach. Once fully qualified, EGT will supplement missile flight tests to gain further insight into flight performance and to support surveillance activities.

Under Navy sponsorship, Draper established facilities and other resources to replicate Trident D5 missile
*****************************************************************************************
environments. An 18,000-sq ft Special Test Facility at Hanscom AFB includes a 32-ft centrifuge capable of controlled high-precision acceleration and an electrodynamic shaker capable of strategic profiles.

Cost Reduction: Guidance Repair Consolidation at the Integrated Support Facility
As part of Draper’s expanded role as Fleet Ballistic Missile (FBM) Guidance Program Systems Integrator, the Laboratory is now responsible for all aspects of guidance system repair. In addition to ongoing 10 PIGA repair at Honeywell in Clearwater, Florida, this responsibility includes management of repair activities at the Integrated Support Facility (ISF) in Pittsfield, Massachusetts. Consolidation of repair activities at the ISF is providing the Navy with current cost savings and will provide superior long-term program support.

Managed by Draper and operated by a General Dynamics/Raytheon team, the ISF provides full capability for inertial measurement unit (IMU) and guidance system electronics repair. Equipped with assembly clean room areas and stabilized test piers, the ISF enables pressure/vacuum testing, system/inertial sensor testing, module testing, optical testing, and vibration and centrifuge testing.

Advancing GN&C: Technology for Reentry Vehicles
********************************************
In addition to maintaining deployed strategic systems and modernizing existing systems, Draper is analyzing the GN&C technology needed to enable Prompt Global Strike (PGS) capability to deliver non-nuclear payloads with high accuracy to virtually anywhere on the globe in less than 1 hour.

Draper has conducted experiments with sponsors to demonstrate some of the technologies needed for PGS. In addition, Draper IR&D studies have been initiated to enable the generation of boost-throughreentry trajectories in near-real time and to provide in-flight target location updates. Proving this guidance capability will provide a technology base for evolving its use on future smaller missiles, such as the Submarine-Launched Global Strike Missile (SLGSM), on tactical submarines such as the SSGN and NSSN.

Contact Information: busdev@draper.com
http://www.draper.com/strategic/strategic.html<\/u><\/a>

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4233
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 09.09.10 14:41. Заголовок: y Chefa Gen.konstruk..


y Chefa Gen.konstruktora Glonass Yrlichicha toze mozete sprosit *

http://rniikp.ru/ru/pages/about/publ/gurnal_b0001.pdf<\/u><\/a>



Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4236
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 09.09.10 15:41. Заголовок: Posle porazenija po..


Posle porazenija pod Belostokom / polnaja poterja swjazi ,mnogochislennie swidetelstwa/ k konzu wojni
iz 12 mln chel Sow. armii pochti 1 mln bili swjazisti
----------------------------------------------------------------

300 kamazow po 100 kwt -1000 kwt moschnost'ju post. pomex kazdij -eto divizija ( po analogii stankowoj diviziej ,kazdij kamaz s pp ,antennoj pri massowom wipuske deschewle tanka )

w mastabax Stalina 10 -40 podobnix divizij ne problema


Budut stawit' pomexi s raznix yglow attaki w neskolkix eschelonnax

pri massirowanom nalete KR s GPS w kombinazii s pomexami ot Yabch ( w 1985 iz 40 000 yabch w SSSR 1500 bilo dlja S-300)

wse texnicheskie reschenija dawno est' -
****************************************

lampi po megawatt na 1.6 ghz s seredini 50 godow ,kamazow i metalla dlja antenn
toze dostatochno .

kwalifikazija srochnosluz. w dannom slushae ne dolzna bit' osobenno wisokoj ( 2 goda srochnoj sluzbi, iz nix polgoda ychebka , + 9 -18
mesjacew kursi w DOSSAF ) -toze wse oprobawanno




Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4361
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 14.09.10 11:29. Заголовок: Xoroschij kommerches..


Xoroschij kommercheskij priemnik

http://www.spirit-telecom.ru/datasheets/SSSR-Whitepaper.pdf<\/u><\/a>

СВЕРХЧУВСТВИТЕЛЬНЫЙ ПРОГРАММНЫЙ НАВИГАЦИОННЫЙ ПРИЕМНИК

opisanie

........

Ne nado tolko wpadat *w illuzii ,chto slozno postawit* pomexi k podobnogo roda izdelijam

diskutiruetsja razbros ot raznix sputnikow 50 db ...

S pomoschju sredstw ykazannix wische (no ne podriw ybch) otnoscheni pomexi k poleznomu signalu na wsode
budet +100 -120 db

ФАКТОРЫ, ВЛИЯЮЩИЕ НА ВОЗМОЖНОСТЬ СПУТНИКОГО ПОЗИЦИОНИРОВАНИЯ
Идеологи и основатели спутниковой навигации 30 лет назад рассматривали решение задачи
позиционирования на Земле в предположении, что сигнал прямой видимости от навигационного спутника
принимается НАП на открытой местности и точность позиционирования зависит только от
фундаментальных причин. К числу последних относятся точность определения орбит спутников
(описывается в альманахе), точность их позиционирования на орбите (описывается эфемеридами),
точность атомных часов на спутниках, искажение пути распространения сигнала через ионосферу и его
учета. В меньшей степени точность позиционирования объекта на Земле или в ближнем космосе зависит
от навигационного приемника сигналов спутников при условии, что при его проектировании и реализации
выполнены основные условия: локальный генератор формирует опорный сигнал с точностью ~10-6, прием
и обработка сигналов спутников согласованы по точности с формированием сигнала на спутнике и
расположением группировки навигационных спутников, внутренние шумы на входе радиотракта по
мощности соизмеримы с мощностью внешнего космического шума на том же входе и пр. При этом
использование внешней по отношению к спутниковому(ым) созвездию(ям) информации, передаваемым
приемнику по каналам связи от специальной службы и/или систем функционального дополнения
(наземного или спутникового) способствует повышению точности навигации.
Энергетические возможности излучающего спутникового радиотехнического оборудования и антенн
рассчитывались, исходя из возможности обеспечения напряженности радиополя вблизи поверхности
земли такой, чтобы мощность сигнала на выходе стандартной антенны составляла -160 дБВт (или, в других
единицах, - 130 дБм), который должен приниматься надежно современным спутниковым приемником.
Именно таковой должна быть чувствительность навигационного приемника, способного принимать и
обрабатывать сигнал навигационного спутника на открытой местности. Первые реализации спутниковых
навигационных приемников 15-20 лет назад для широкого использования обеспечивали чувствительность
на уровне -160...-165 дБВт (-130…-135 дБм), которая позволяла успешно принимать сигнал
навигационного спутника указанной мощности и в то же время позволяла базироваться на современном
уровне микроэлектроники.
Снижение этой мощности в силу разных причин (прохождение радиоволны через листву дерева, дождевую
тучу, крышу или стену здания, эстакаду, под которой проходит человек или проезжает поезд или
автомобиль, и многое другое) может ослаблять интенсивность радиосигнала и драматически влиять на его
прием, а, значит, прерывать вывод навигационных данных и даже полностью парализовать работу
спутникового навигационного приемника.
Если же оценить мощность такого радиосигнала за обычным стеклом, то, как показали эксперименты,
ослабление сигнала составит 1-4 дБ, за деревом – на 2-9 дВ в зависимости от толщины стены, за толстым
стеклом со свинцовыми добавками – на 8 - 20 дВ, за бетонной или кирпичной стеной - на 12-43 дБ
(например, при толщине бетонной стены 25 см – на 20 дБ или в 100 раз), т.е. приемник должен принимать
сигнал мощностью -180...-200 дБВт. Многие исследователи отмечают, что при ослаблении сигнала на 25
дВ и более, становится невозможным осуществить нормальный прием без дополнительной поддержки
типа Assisted GNSS (наиболее известна Assisted GPS), когда навигационный приемник получает
дополнительную информацию о времени и орбитах спутников по каналам сети мобильной связи или через
Интернет. Наличие дополнительной информации в начальный период работы приемника и/или в
стационарный интервал времени его функционирования сильно влияет на характеристики «холодного»
старта, «горячего» старта, «повторного горячего» старта, т.е. уменьшает время старта за счет уменьшений
времени поиска сигнала на плоскости «время (задержки) – частота (Допплера)», что является весьма
важным для разных приложений, а для некоторых даже критичным.
Из этих сведений понятно, что особо затруднен прием радиосигнала внутри помещения. Предъявить
требования к надежной работе приемника в таких условиях крайне сложно в силу большого разнообразия
возможных сценариев. Как правило радиосигнал внутри помещения не только ослабляется крышей,
стенами, оконными стеклами, но и приходит после отражения от зданий и других объектов, претерпевает
многочисленные переотражения внутренними перегородками и пр., что значительно ослабляет его
мощность на входе приемника. Следует считаться также со значительным разбросом уровней сигнала от
отдельных спутников, способном достигать 50 дБ и более даже в помещениях с большим количеством
окон. Стеклянные стены современных офисов, отелей и бизнес центров, несмотря на кажущуюся
радиопрозрачность, также вызывают значительное снижение мощности радиосигнала. Затухание
радиосигнала при прохождении через толстое стекло с большим содержанием свинца сопоставимо с
аналогичным показателем кирпичных и железобетонных стен. Работу навигационного приемника внутри
таких “стекляшек” можно сравнить с навигацией в помещении без окон.
Подобная ситуация может возникать в местах парковок под зданиями, внутри многоярусных гаражей,
внутри молов и торговых центров и т.п.

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4362
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 14.09.10 11:40. Заголовок: Один из подходов в е..


Один из подходов в ее решении – сверхчувствительные программные
навигационные приемники для мобильных приборов (нетбуков, смартфонов, коммуникаторов, MIDов и
др.), подключенных часто к Интернету и имеющих в своем составе мощный процессор, на который
обычно возлагается поддержка ряда приложений. Такие приемники будут очень скоро представлены на
рынке навигационных устройств и в статье описано одно из пионерских решений в этой области,
которое обеспечивает позиционирование не только вне помещений, но и внутри их благодаря
разработанным алгоритмическим ухищрениям и ноу-хау.


сверхчувствительные -eto objazatelnoe marketingowoe ponjatie dlja massowix potrebitelej ...

chto to dolzno bit swerx... ,exclusiv - inache ne prodat ...


-----------------------------------------------------------------------------------------------------


1 .Diapazon ,diametr antenni-antenn , koef .ysilineija ,podawlenie bokowix lepestkow ,ee schumowaja temperatura
2 .Schumowaja temperatura priemnika ,ispolzowanie kriogenowgo oxlazdenija


Moschnost* izluchenija spuitnika w predelax 5 kwt (battarei) 10 kwt ,antenni w otlichii ot Milstar/AEHF nenaprawlennie
w sluschae dalnejschego prim napr. ,diapazon xuze 1.5 ghz protiw 20/44 ghz y Misltar

rasstojanie do sputnikow 20 000 -40 000 km , do postanowschika pomex 200 km ( kwadratichno 100 raz w kwadrate=10000)

antenni postawschikow pomex mogut bit ostronapr. s diamtrom po 3-4 metra Moschnost - 10kwt -1 megawatt




Спасибо: 0 
ПрофильЦитата Ответить



Сообщение: 3
Зарегистрирован: 29.08.10
Репутация: 0
ссылка на сообщение  Отправлено: 16.09.10 21:17. Заголовок: честно говоря вопрос..


честно говоря вопрос остался открытым... жаль что именно спецов здесь не нашлось

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4434
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 16.09.10 22:21. Заголовок: Lans -честно говоря..


Lans -честно говоря вопрос остался открытым... жаль что именно спецов здесь не нашлось
*******************************************************************************

W chem otkritim ?

1. Wichistit* wam primitiwnuju pop propagandu iz mozgow ?
--------------------------------------------------------------------

Eto wam nikto delat* ne budet -s wisokim chansom bessmislenno
------------------------------------------------------------------------------

2. Wische ykazanni adressa /na web stranize prisutstwujut tel i e-mail/ Glaw .konstruktora Glonass RNIIKP,
shefa konstruktora Spirit telekom ,Draper laboratory , razrabotchikom ECCM dlja F-18 -F-35


Obraschajtes* wam raz*jasnjat detali ,kotorie puiblichni


Neowzmozno postawit* nabor zabluzdenij i pop mnenij ,kotorimi wi operiruete
********************************************************************
w centr mirozdanija
*****************


Wsex yspexow ...

P.S. No popitajus wam otwetit* wpredalx waschego pop musora w golove

Собственно интересует, возможно ли на нынешнем этапе эффективное подавление военных GPS приемников?

da
---
С одной стороны подобные разработки есть и рекламируются,

kakie ? dlja podawlenija pop Glonass za 150$ ili dlja woennie ?

w woennix ECM berite smelo srednujuu moschnost* minimum 10 kwt

grafik sootnosschenija pomex / k poleznomu signalu dlja nenaprawlenennoj antenni priweden wische

w tom chisle i dlja 100 km i dlja 10 kwt ( eto ne predel)



но "спецы" работающие с GPS говорят,


Kto iz nix spec ? Glawnij konstruktor RNIIKP ? Wi s nim besedowali ? Pozwonite i sprosite
****************************************************************************

Ili awtor postinga dolzen eto delat* za was ?
**************************************
что заявленные для таких систем дальность подавления в 100-150 км реальны только для гражданских изделий и для военных приемников эти значения будут составлять не более 150-200 метров.

Dlja kakogo postanowschika pomex ? Dlja togo ,kotorij bil razrabotan dlja podawlenija pop priemnikow za 150 $

Ili iz komplekta S-400 ? Poslednij budet imet* srednjuu moschnost* minimum 10 kwt i skoree wsego naprawlennuju antennu

Smotri grafik wische Draper laboratory dlja nenapr. i 10 kwt

То есть, по факту, против ВТО с системами спутниковой коррекцией не эффективны.

Woennie ,razrabotannie dlja podawlenija w sostawe s-300/400 effektiwni

Sr. moschnost S-300V 10 kwt ,y S-400 mozet bit* i 100 kwt

+ naprawlennaja antenna ( pribawte Ky )

**************************************

Powtor

ykazanna wozmoznsot* raboti woennogo priemnika pri signale pomexi na 40 db prew. poleznij signal

na grafike na ris 8 pri signale pomexi 10 kwt i nenaprawlennoj antenne
*************************************************************

signal pomexi na 70 db bolsche na rasstojanii 100 mil (160 km)
**********************************************************

Chto ne jasno ?
************
************

Wasche pop mnenie i "speci" ne soglasujutsja s mneniem Draper laboratory ?
******************************************************************

Wi ne znaete chto takoe prewischenie signala pomexi na wxode nad poleznim 70 db na rasstojanii
*********************************************************************************
160 km dlja 10 kwt i nenapr. antenni ?
**********************************

Ili wi predpolagaete ,chto skonstruirowat* priemnik GPS dlja woennogo primenenija
bez naprawlennoj antenni s malimi gabaritami ,kotorij moschet otfiltrowat* pomexu
po yrownju wische poleznogo signala na 70 db( 10 mln raz po moschnsoti) eto
prostejschaja zadacha ?

70 db na grafike na ris 8 dano dlja 10 kwt moschnsoti pomexi i 160 kilometrow rasstojanija


Ili wam nuzno prepodnesti w stile -super -swerx ,Putin , Russkaja duxownost* ,nanotexnologija
*********************************************************************************
Rossija wpered ,amerikosi ,2 palza wwerx ..
******************************************

Obraschajtes* w www.kp.ru na blog polkownika Baranza ,on specialno dlja takix kak wi ,wam budet komfortno
w ego kompanii







Draper laboratory - stat*ja o pomexaxwoennim GPS priemnikam

http://www.draper.com/digest97/paper5.pdf<\/u><\/a>

Nominal GPS level L2 -166dbw

smotri grafik 8

signal GPS s moschnsot*ju 10 w -16 mozet bit* ispolzowan pri nalichii moschnsoti pomex 10 w -12

t.e. 40 db raznici .mozno sdelat* boslche chem 40 db bez problem


Ogranichennost* GPS

1. Rasstojanie 20 000 km protiw istochnika pomexi w 100 raz blize = 200 km

snizenie rasstojanija w 2 raza = ywelicheniju moschnosti w 4 raza

w 100 raz -w 10 000 raz

2. Antenna peredatchika i priemnika ne naprawlena i chastota dowlno newisokaja 1.5 ghz


3. Moschnost* peredatchika sputnika ( moschnsot* battarej do 10 kwt w lutschem sluchae)

4. Moschnost* peredatchika pomexi mozno bez problem sdelat * 100 kilowatt -1 megawatt (na chassi
YAZ-Tigr-Kamaz - z/D Vagon) .Antennu naprawlennoj

1.8 metra 1.5 ghz eto 6.5 grad schirina lepestka

*************************************************

ykazanna wozmoznsot* raboti woennogo priemnika pri signale pomexi na 40 db prew. poleznij signal

na grafike na ris 8 pri signale pomexi 10 kwt i nenaprawlennoj antenne

signal pomexi na 70 db bolsche na rasstojanii 100 mil (160 km)
**********************************************************

100 kwt -budet na 80 db (limit raboti woen. priemnika 40 db)
1 megawatt -budet na 90 db

+ Ky naprawlennoj antenni

pri diametr 4.8 metra gain dlja 1.6 ghz budet primerno 36- 37 db
****************************************************

http://www.gdsatcom.com/Antennas/Data_Sheets/6550034D_4.8m.pdf<\/u><\/a> (ykazan dlja 3.6 ghz -44 db ,dlja 1.6 ghz
otnjat 7-8 db)








Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4436
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 17.09.10 12:03. Заголовок: Предположим теперь,..


Предположим теперь, что в качестве постановщика помехи используется современный цифровой глушитель. По словам директора российского ООО « Авиаконверсия » Олега Антонова: «Цифровой глушитель нового поколения, получив часть навигационного радиосообщения, запоминает его и затем многократно повторяет в эфире. Такой метод постановки помехи продемонстрировал очень высокую эффективность». Опробуем его действие на предлагаемом детекторе (Рис.6).


Разумеется, что как только соотношение сигнал/помеха ухудшится, приемник будет выведен из строя,
*****************************************************************************************

Na 70 db ... na rasstojanii 160 km s reservom

1.powischenija otnoscheniaj schum/signal do90 db ( 1 megawatt) i do 125 db (napra atnenna 4.5 metra -5.4 metra)
2. Ispolzowanija podriwa neskolkix serij po 16-32 yabch ( w Sowetskoe wremja iz 40 000 yabch 1500 bili dlja s-300)


Poka ne widel ni w odnoj disskusii otnoschenie pomexa/signal 70 db ...

Najdu skazu .. .


т.е. современный глушитель значительно эффективнее простейшего.

http://www.tredex-company.com/article_show.php?id=11<\/u><\/a>

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4437
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 17.09.10 12:08. Заголовок: 7 Februar 2008 ..


7 Februar 2008 | АвиаПорт.Ru
Российские специалисты ищут способы противостоять развертыванию в Восточной Европе систем ПРО.

Российские специалисты ищут различные возможности противостоять развертыванию в Восточной Европе (Польша и Чехия) систем противоракетной обороны (ПРО), направленных исключительно против России. Своим видением этой проблемы в беседе с корреспондентом "АвиаПорт.Ru" на выставке "Беспилотные многоцелевые комплексы в интересах ТЭК" поделился директор ООО "Авиаконверсия" Олег Антонов.



"Одной из мер противодействия американской ПРО, а также авианосным соединениям, является создание помех станциям управления и фактически подавление их функционирования", - полагает собеседник.



По его словам, компания впервые озвучила методы борьбы с базами ПРО, а также американскими авианосцами, на авиасалоне в Ле Бурже в 2007 году. "Впервые компания продемонстрировала натурные образцы передатчиков помех GPS и ГЛОНАСС на МАКС-2007 и только тогда американцы оценили, какая это "бомба" под их высокоточное оружие", - сказал О.Антонов.



Он напомнил, что ранее системами постановки помех измерялись параметры сигнала, передаваемого "заглушаемым" излучателем, параметры "запоминались" и потом ретранслировались системой постановки помех. Однако, по словам собеседника, с конца 70-х годов реализуется совсем другой принцип. Сегодняшняя система помех постоянно находится в режиме приема, не обрабатывает сигналы, а запоминает их и передает их, наделяя ложной информацией. "Суть создания помех состоит в том, что помеха - ответная. То есть принимается сигнал, он запоминается и переизлучается без каких-либо изменений, но при этом ответный сигнал наделяется ложными целями, многими разными траекторными признаками с тем, чтобы наши ложные цели ничем не отличались от реальных целей", - уточнил глава компании.



О.Антонов по просьбе "АвиаПорт.Ru" прокомментировал эффективность использования системы постановки помех на опыте второй Иракской кампании. "США знают ООО "Авиаконверсия" по скандалу начала войны в Ираке, когда 10 дней американские ракеты и бомбы в цели не попадали. На пятый день "иракской кампании" США прислали России ноту, однако "Авиаконверсия" доказала, что продали станции помех посредникам", - сказал О.Антонов. Он добавил, что США до войны в Ираке были лучшими покупателями и закупили у российского предприятия несколько десятков постановщиков помех для изучения и испытаний своего оружия.



Menee werojatno ,chto dannie stanzii imeli srednjuu izluchaemuju moschnsot 10 kwt ( 70 db pomexa/signal na 160 km)

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4438
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 17.09.10 12:59. Заголовок: na linke foto GPS ..

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4439
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 17.09.10 13:11. Заголовок: http://www.gmat.unsw..


http://www.gmat.unsw.edu.au/snap/publications/dempster_2005a.pdf<\/u><\/a>


2. Why is GPS Vulnerable?
The real problem here is that the signals received from a GPS satellite are extremely
weak. The transmitter power is 27W (equivalent to a weak light bulb) and it is at least
20,000 km away! The signal on the ground is so weak (10-16 W or -160dBW) that it
sits 20dB below the background noise level. This means that if you try and “see” it by
scanning the spectrum, you won’t notice anything. Special signal processing hardware
(called “correlators”) is used to bring that signal above the noise within the receiver so
that it can be used to make measurements. In radio applications, if the signal is not
above the noise, it isn’t useful. Tracking such low-power signals is difficult, but
acquiring them (i.e. finding them within the background noise in the first place) is


even harder - requiring a further 6 – 10 dB of signal-to-noise ratio. (ANDREW, I
suggest a sentence here defining “dB”, as some readers will not have that
background…..)
Now, if there was another signal that was also received in the same frequency band,
that signal does not have to be very strong, only 30-40dB stronger than GPS,
****************************************************************
for it to
“out-punch” the GPS signal.
************************


Awtorwische ykaziwal 70 db dlja 10 kwt na 160 km ,nenprawlennoj antenni (source Draper laboratory)

s wozmoznost*ju dalnejschego powischenija do 90 -125 db (megawatt i 4.5-5.4 metra antenna)


Dlja sprawki S-500/400/300 imejut w swoem sostwe raznei dop. RLS s moschnost*ju 10 -100 kwt

k primeru Nebo RLS dlja detekzii VLO ,stanzija pomex na 1.5 ghz 10 -100 kwt i antennoj diamtrom
3 metra na chassi KAMAZA budet ne doroze
----------------------------------------------------

Cassegr. antenna sraznimi ysiliteljami daet womoznost* postanowki pomex w diapazonax 1.5 -44 ghz


The source of such a signal is called a “jammer” and the
process of preventing GPS from working is called “jamming”. A jammer does not
have to be a very powerful signal transmitter. For instance, a 0.1W transmitter can
prevent the acquisition of GPS signals across an area with a 10km radius.

Спасибо: 0 
ПрофильЦитата Ответить



Сообщение: 4
Зарегистрирован: 29.08.10
Репутация: 0
ссылка на сообщение  Отправлено: 18.09.10 15:07. Заголовок: спасибо :sm36: жал..


спасибо
жаль только с английским трудно

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4485
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 20.09.10 21:09. Заголовок: Rockwell Collins adv..


Rockwell Collins advances next-generation GPS by tracking new military signal


CEDAR RAPIDS, Iowa (February 02, 2010) - Rockwell Collins recently achieved live satellite M Code tracking with its new Global Position System (GPS) receiver for the Modernized User Equipment (MUE) program, marking a major step forward in developing the next generation of GPS technology for the military.

The MUE receiver card development program, awarded to Rockwell Collins in 2006 by the U.S. Air Force Space and Missile Systems Center (SMC), is developing the military user equipment portion of the next-generation GPS system that incorporates a new military signal and security architecture. The new technology offers enhanced integrity, exclusivity and improved anti-jam capabilities.

M Code, which stands for Military Code, is a key element in the modernization of military GPS. While it is transmitted on the same L1 and L2 frequencies used by the legacy P(Y) Code, it will significantly improve the security of military GPS. The ability to track the new code by the modernized GPS receivers is an important milestone for the MUE program.

"Pioneering GPS technology has long been a core competency for Rockwell Collins, dating back to our involvement in the development and launch of the Navstar Global Positioning System in the 1970s," said Ron Hornish, vice president and general manager of Precision Strike Solutions for Rockwell Collins. "Our success with the MUE program is indicative of our heritage and expertise in developing new GPS solutions that will deliver heightened security and performance to the military."

Rockwell Collins (NYSE: COL) is a pioneer in the development and deployment of innovative communication and aviation electronic solutions for both commercial and government applications. Our expertise in flight deck avionics, cabin electronics, mission communications, information management, and simulation and training is delivered by nearly 20,000 employees, and a global service and support network that crosses 27 countries. To find out more, please visit www.rockwellcollins.com.



Media Contact:
Pam Tvrdy-Cleary
319.295.0591 office
319.431.0951 mobile
pjtvrdy@rockwellcollins.com



http://www.seos.co.uk/news/page12256.html<\/u><\/a>

Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4486
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 20.09.10 21:12. Заголовок: GPS Modernization C..


GPS Modernization
Col. Dave Madden Looks Back, and Forward into GPS Future
July 27, 2010 By: Don Jewell GPS World
************************************


GPS Wing Commander Gives Outgoing Interview
********************************************

I had the honor of attending Colonel David Maddens’ retirement luncheon at the Space and Missile Systems Center (SMC) on Los
***********************************************************************************************************

Angeles Air Force Base (LAAFB) on June 16, and it was quite an event. Just prior to it, I asked Dave if he would like to conduct an exit interview after he took a short vacation with his family. He agreed it would be a good idea and a way to say some things he has wanted to say for awhile.



During the retirement luncheon, various people and organizations presented Dave with mementos of his time at the GPS Wing; I stopped counting at approximately 50 different presentations. This is an indication of the high regard in which Dave is held by those with whom he works on a daily basis. The military shadowbox he was presented (see photo), which is a typical military farewell presentation, had the following inscription, which is certainly not typical, and sums up the way those who work with Dave feel about him as a commander and as a person.

"It is not the critic who counts: not the man who points out how the strong man stumbles or where the doer of deeds could have done better. The credit belongs to the man who is actually in the arena, whose face is marred by dust and sweat and blood, who strives valiantly, who errs and comes up short again and again, because there is no effort without error or shortcoming, but who knows the great enthusiasms, the great devotions, who spends himself for a worthy cause; who, at the best, knows, in the end, the triumph of high achievement, and who, at the worst, if he fails, at least he fails while daring greatly, so that his place shall never be with those cold and timid souls who knew neither victory nor defeat."

Theodore Roosevelt
"Citizenship in a Republic,"
Speech at the Sorbonne, Paris, April 23, 1910

Dave was officially retired the next day by Colonel (USAF, retired) Bradford Parkinson. Dr. Parkinson was the first GPS Joint Program Office Director, in the early 1970s. He recently reviewed those early days and those responsible for the success of GPS with a two part series in the pages of GPS World.
Interview

Don Jewell (DJ): Dave, after almost four years first as the Vice Commander and then for the last three years the commander of the GPS Wing, of what are you most proud?

Colonel David Madden (DM): Overall, the GPS Wing has made significant progress over the years moving critical space system developments and acquisitions forward. The GPS Wing continues to lead with a “back-to-basics” foundation of rigorous system engineering, incorporated strategies like parallel risk reduction and capability insertion efforts, incremental delivery of timely and valuable capabilities to warfighters and civil users, and best business practices with solid cost estimates and contract incentives. Our new GPS III space vehicle, Next Generation Control Segment, and our GPS Modernized User Equipment programs incorporate our latest thinking of these innovations, and pave the path as a model for future acquisitions: low risk and high confidene associated with program execution (cost, schedule and technical performance).

The GPSW Team has had many specific accomplishments over the last four years. I would like to highlight just a few.

Space Segment. In the space segment, we accomplished a major milestone in GPS history with the launch of the final GPS IIR-M satellite in Aug 2009. GPS IIR-21 (M) marked a critical milestone in the GPS modernization program that was initiated in early 2000. The GPS IIR/IIR-M satellites are the cornerstone of the GPS constellation, and I expect them to perform well into the future. We’ve completed the development, testing and launch operations of the first GPS IIF Space Vehicle. The GPS IIF is the “Dawn of a New Era” of GPS services, providing new and improved capabilities that will continue to support not only the warfighter but commercial and civil users around the globe. IIF vehicles two and three will be delivered by early 2011, and two of the remaining nine fixed-priced vehicles are already proceeding down the Boeing Pulse Line.

Another noteworthy accomplishment was the award of the GPS III spacecraft contract. The GPS III will be developed in three increments with each increment to include more capabilities based on technical maturity. We successfully completed the GPS IIIA satellite Preliminary Design Review (PDR) in May 2009 and the GPS IIIA Critical Design Review (CDR) is scheduled for August 2010, two months ahead of schedule, which completes the detailed design and lays the foundation for fabrication. GPS IIIA is a back-to-basics spacecraft program with a strong focus on systems engineering, mission success, and acquisition excellence.

Ground Segment. In the GPS ground control segment, great lengths were taken to ensure the successful replacement of the decades-old command and control (C2) system with the new Architecture Evolution Plan (AEP) software, to improve GPS operator interfaces while providing a test capability for the new signals on the modernized satellites and to improve launch, anomaly, and disposal (LADO) operations. This new software will also provide robust security improvements to include “over-the-air” distribution (OTAD) of encryption keys to properly equipped military users.

I would also like to mention the successful award of the Next Generation Control Segment (OCX) back-to basics contract. The current acquisition strategy for fielding the OCX consists of four increments (commonly referred to as Blocks). The recently awarded OCX contract consists of Blocks one and two [while] Blocks three and four will be follow-on contracts that align with the future GPS IIIB and GPS IIIC spacecraft capabilities.

User Segment. In the GPS user equipment segment, we are actively working the development of a new generation of military user equipment to take advantage of the modernized M-Code [military only] signals. Currently we are conducting technical demonstrations and risk reduction for our next generation Military GPS User Equipment (MGUE) and defining a creative acquisition strategy.

USD-AT&L (the undersecretary of Defense for Acquisition, Technology and Logistics) signed an acquisition decision memorandum (ADM) on May 24, 2010, approving a material development decision for MGUE: the formal entry point for MGUE into the acquisition process. Currently, our three Military User Equipment (MUE) contractors are testing and delivering prototype cards this summer; government testing follows.

The foundation of our MGUE acquisition strategy is an incremental approach that leverages technology developed under the MUE program to move into engineering and manufacturing development of the first MGUE receivers as soon as possible. The strategy will be submitted to the Pentagon this summer after SMC coordination and PEO Space approval.

Our business strategy over the long term is to develop common GPS modules (CGMs) as the core engine for all DoD user equipment. We will develop CGMs incrementally as well, to support the form factors for the air, maritime, and ground domains. By early fall, we will have a final technical requirements document (TRD) for the MGUE form factors and CGM. We expect an RFP release in Feb 2011, and a Milestone A in May 2011. By early FY12, we should be on contract for Increment One of MGUE.

System Sustainment. From a systems sustainment standpoint, our GPS Wing detachment located at Peterson AFB has exceeded all expectation associated with ground (software and remote sites), user, and satellite systems sustainment. Even with all the system upgrades over the past year our sustainment team has kept the operational system performance well above the requirement: Read, no capability impact to civil or military users.

In fact, performance (availability, accuracy, and integrity) has been significantly improved over the last four years. Finally, they are normalizing sustainment of the current user equipment (DAGR-Defense Advanced GPS Receiver, MAGR-2K-Miniaturized Airborne GPS Receiver Version 2, and ADAP-Advanced Digital Antenna Production program) by transitioning sustainment responsibility to Air Force Material Command, specifically the Warner Robins Air Logistics Center depot at Robins AFB, Georgia.

Partnerships. The GPS Wing has established a close working relationship with Air Force Space Command Headquarters at Peterson AFB, Colorado for overall system operations, sustainment, and development responsibility; the 45th Space Wing (launch operations teams at Cape Canaveral Air Force Station in Florida), the 50th Space Wing (Overall System Operators at Schreiver AFB in Colorado), the Launch and Range Systems Wing (Los Angeles, California acquisition organization with responsibility for getting our GPS satellites successfully to orbit), the United Launch Alliance, the many government agencies (FAA, DOT, DOE, NSA, NGA, NASA, and so on), OSD organizations (PA&E, NII, AT&L, DOT&E), and our dedicated and professional prime contractors and major subcontractors to successfully sustain and enhance GPS mission capabilities — providing the highest overall daily system availability and the most robust GPS on-orbit constellation ever for war fighters and civil users worldwide. The constellation is healthier than it has ever been, and with the launch of the first IIF satellite and the on-track development of GPS IIIA, we are poised to maintain GPS as the gold standard for positioning, navigation, and timing well into the future.

The People. Finally and most importantly, I am proud of the men and women that make up the GPS Wing. They have molded many players (Aerospace, MITRE, service reps, international officers, government and civil agencies, SE&I and SETA (support) contractors, and U.S. Air Force military and civilians) into a finely tuned machine that is always focused on the number one priority: mission success. At the same time they have made the Wing a fun place to work. The GPS Wing members have made significant contributions to the quality of life in the GPSW, on LAAFB (Los Angeles Air Force Base), and the local community. Whether it was the great Company Grade Officer Association activities, tasty Tuesdays, the BBQs by the base gym, the holiday parties, the POW/MIA (Prisoner of War/Missing in Action) Run, the yearly toy contributions to the Marine Corp Toys for Tots program, regular food drives to support the Redondo Beach community, the yearly car show, the GPS Partnership Council, GPS University, or the many visits to local schools (just to name a few activities), they are truly a class act of which I was honored to be a small part.

DJ: Dave, how would you most like to be remembered?

DM: As the "AGER" guy. The one who put the enterprise back together, which will lead to better synchronization among the segments and ultimately deliver future warfighting capability to the U.S. and Allied forces. Senior AF, DoD, and Congressional leadership now look at GPSW execution as a enterprise rather than a collection of individual ACAT 1D (Acquisition Category 1D) programs. This has allowed the modernization program to move forward, significantly reducing the numbers of reviews, documents, and decision complexity.

DJ: Dave can you explain just where we are today in the ongoing GPS-IIF saga? Are we on track and on schedule to have IIF-1 activated sometime in late August? Will there be a second IIF launch this calendar year? Does Boeing finally have it all together?

DM: Don, I'm actually glad you asked the question that way, because it gives me an opportunity to address it squarely. It is completely fair to call the GPS IIF program a saga because of how long it took us to get to our first launch. But it is also important to ensure the credit and blame gets spread properly. The program did suffer from the sins of acquisition reform in the 1990s — on the government side and the industry side —- as well as major requirements changes years after program initiation. In hindsight, I'd have to say that we collectively failed again in the mid 2000s when we were overly optimistic about the time and funding needed for the challenges we would face in recovering from TSPR (Total System Performance Responsibility). On the flip side, during my tenure here I've had great support from my senior leadership — and from their Boeing counterparts — for taking the time necessary to ensure we have a quality program. We kept our eye on mission assurance and fixed quite a few end-of-life risks. We might not have had that luxury if the constellation weren't so robust over the past few years.

In the end, the proof is in the on-orbit performance. So far, I'm proud to say that the checkout of SVN-62 has been proceeding very smoothly. My guys and Boeing have a great working relationship with the crews up at the 50th Space Wing, so the bird is in good hands. I expect we'll find a few things we want to tweak before making the satellite available to users [Editors Note: See An L5 Surprise]. Most space programs do that with the first satellite of a kind. In the end, the users will have a satellite that adds real benefit to the constellation performance.

Right now the teams are still pushing hard to get SV-2 ready to launch. There are still a few hurdles to clear, and the leadership needs to evaluate whether or not the constellation really needs another GPS IIF just yet or can it wait until next summer. I would love to watch another one go up this year, but it just won't be the same watching from the sidelines!

DJ: I know it won’t be the same, Dave, but it should still be exciting. Now how about an update on the OCX program and how it is progressing?

DM: The OCX program is off to a great start. We awarded the contract to Raytheon in February 2010 and kicked off the integrated baseline review (IBR) in March. We are currently working side-by-side with Raytheon to solidify the program management baseline so we can jointly manage the program in a back-to-basics manner. Phase B software development for controlling modernized features is underway and builds on Phase A products, which we demonstrated with a prototype in December 2008. I have tremendous confidence that the OCX program will deliver promised capabilities on time to support modernized GPS.

DJ: Can you give us an update on where we are with the GPS IIIA program? Have you been successful in maintaining the no-changes mandate?

DM: GPS IIIA has maintained a stringent, back-to-basics approach since program inception. This has included significant investment in early systems engineering, and strict requirements discipline. To date, no new requirements have been levied on the GPS IIIA. Any new requirements for consideration are being addressed in future blocks as planned. The program is currently on track, and is forecasting the completion of Critical Design Review 60 days ahead of the baseline schedule.

DJ: We have satellites on orbit today that will reach their mean mission duration without broadcasting all resident signals or using all capabilities? Is there a plan to address this issue?

DM: Although there is some concern that the IIR-M satellites may reach their end of life before the L2C capability has been deployed, or that the IIF satellites may reach their end of life before L5 has gone operational, the concern is not justified by our reliability predictions and our current program plans. Current plans are for OCX Block 1 to provide L2C support, which is projected in the August 2015 timeframe, whereas the IIR-M satellites are expected to live well into the 2020 timeframe. Likewise, OCX Block 2 will provide L5 support in the 2016 timeframe, and our IIF satellites are expected to live into the 2025 timeframe. Therefore the likelihood that IIR-M or IIF satellites will be decommissioned before L2C or L5 have become operational, respectively, is very low.

Over the last couple of years, lots of discussion has gone into the integration issue, but I am not really sure what providing fully integrated GPS capability really means. What I do know is the user needs all three segments (satellite, ground command and control, and user equipment) to fully utilize new system capability. I also know that system integration comes in two forms. First and foremost from a technical design standpoint. This allows individual segments to be delivered independently but with high confidence the system will operate when all three elements arrive. This gives flexibility to the dynamics associated with budgets, policy decisions, requirements changes, unexpected technical hurdles, launch availability, and weapon platform availability for integration and testing (just to name a few variables). Rest assured the GPS enterprise is integrated at the technical level. However, it’s the second form of integration that gets all the attention: having all segments delivered in a reasonable proximity to each other. Not to make excuses, but as it relates to GPS, this is just hard to accomplish because it involves a span of control and accountability that is almost infinite. Many in the community recognize this reality, which has allowed the Air Force to set appropriate and realistic expectations so real capability can be delivered.

That being said, there are prudent things that can and are being done to speed the deployment of capability and set appropriate expectations. The most significant has been to broadcast the M-Code, L2C, and soon L5 signals from space to allow civil and military user equipment manufacturers to begin development and testing of their next generation of receivers. This gives industry a jump while the U.S. Air Force continues to develop the C2 capability and the next-generation signal monitoring capability (required to ensure signal in space performance integrity). Also, building the modernization programs with a strong mission assurance foundation is a major step forward. We understand the lessons learned that established the baseline for the current Block II systems delivery; the Block III systems are built on a solid acquisition strategy of reduced risk and increase execution confidence.

DJ: What do you see as one of the biggest GPS enterprise challenges, and what are some of your thoughts on the way ahead?

DM: That’s easy, Don: ensuring global PNT services are not interrupted as the United States continues to modernize GPS. If we don’t continue to develop a more robust means of ensuring user equipment compatibility, even a small number of non-system-compatible receivers (military or civilian) can significantly delay the delivery of critical modernized capability for everyone. Let me explain and provide some thoughts.

Since its initial design in the early 1970s, GPS has evolved in both capability and complexity. In the early days, systems engineering across the space, control, and user segments was relatively straightforward. The GPS Joint Program Office developed all military user equipment, and was able to rigorously ensure all specifications were verified prior to fielding. Over the past 20 years, however, GPS has become ubiquitous throughout the Department of Defense, with tailored satellite navigation solutions developed and acquired by dozens of program offices to support hundreds of unique requirements. Meanwhile, commercial GPS is one of the foundations of the Information Age, with GPS receivers produced in quantities approaching half a billion devices per year. The model of simply providing policies, standards, and interface control documents without providing a means to certify receiver compliance is becoming more challenging due to the continued growth in both military and civil applications for PNT, the competitive nature associated with user system applications and performance, and the increased complexity of GPS. Furthermore, it is especially difficult fielding upgrades to an established system like GPS while maintaining backwards compatibility with previously fielded equipment. These challenges are further exacerbated by difficulties associated with synchronizing the lengthy timelines associated with fielding ground-segment, satellite, and user equipment upgrades.

Recent highly isolated incidents, involving civilian and military receiver and other manufacturers, have highlighted the significant impact a very small number of receivers experiencing compatibility issues can have on the entire enterprise of worldwide users. In addition, a number of cases associated with improper receiver integration into major weapon systems have delayed system fielding as well not allowed the weapon system to best optimize GPS to the overall weapon systems performance.

Therefore, it is my opinion, to ensure worldwide PNT services are not interrupted as we continue to modernize the GPS, a more robust means of ensuring compatibility needs to be explored. (I would like to stop and make a note here: by “we” I mean all the DoD and civil agency stakeholders.) This means we need to not only continue to release “building codes” but we need to develop a capability to be more involved in the development, integration, and testing of new military and possibly civil user equipment.

We have recently taken a number of big steps in this direction.

First, we are currently significantly increasing the number of civil and military GPS receivers in our government testing labs. This will enable us to run tests against a wider variety of receivers, to gain higher confidence before we deploy system upgrades.

Second, we recognize that we need to ensure that our signal specifications, for both military and civil users, are as clear as we can make them. User-community representatives are already encouraged to be full participants in appropriate interface-control working groups. We further recognize that there is no substitute for thorough testing, and hence fully appreciate the importance of deploying signal-in-space capabilities as early as possible, on predictable schedules, so user equipment can be field-tested prior to market release or operational deployment.

Third, we are developing new upgrade fielding methodology whereby when we deploy system upgrades, we will take a more methodical approach and, whenever possible, field upgrades to smaller segments of receivers to prove compatibility without exposing all operational assets simultaneously. We will also apply a new software sustainment model to future military GPS user equipment, to ensure that inevitable system changes are systematically and rigorously executed with minimal impact on DOD programs.

Finally, we are investigating the establishment of something similar to an underwriters laboratory service to help support military programs with integrating GPS into their weapon systems during development. The teams associated with such lab services would support program design reviews as well as help develop the validation criteria for overall system acceptance. In addition, we are also starting discussions with key GPS civil receiver developers on how we might be able to provide a similar service to commercial receiver developers (potential fee-for-service type model).

Don, I highly recommend we continue to develop the four efforts I just mentioned but also dedicate significant time to critical thinking events to ensure we have minimized the risk of a widespread receiver issue, delays in delivering modernized capabilities, or sub-optimized weapon system performance. Manufacturers of equipment adversely affected by recent GPS upgrades have significantly stepped up their interactions with the GPS program office to resolve the compatibility issue and are playing a major role in providing an upgrade to their affected receivers to correct the issue. To date, no operational weapon systems have had to be grounded or civil capability degraded. I encourage the GPS community to treat recent events as a call to arms. GPS has become a critical national and international utility but it is much more complex than the electric or telephone services. How military or civil GPS receivers are designed, developed, and integrated into systems has a significant impact on the overall performance or lack of performance of the system. Don’t let recent events be a lesson not learned; let’s lead and solve the risk before it becomes an issue.

DJ: These are all excellent ideas, Dave, and many of them we have discussed in the past as concepts. It sounds like many of them are now a work in progress, but since you won’t be around to shepherd them into fruition, just what sort of prudent advice would you give Colonel Bernie Gruber as he assumes command of the GPS Wing?

DM: First and foremost, listen to your people — we have a great team! They are skilled professionals who really care about GPS. Second, keep the MGUE program focused and moving forward.

DJ: I certainly hope at a minimum that Bernie listens to your advice on MGUE. Now, Dave, when will the GPS Wing transition back to a Joint Program office, and what affect will this have on the military personnel working GPS? Will this re-designation be detrimental to their careers and future plans for the JPO? Will it lessen the GPS Wing’s/JPO’s influence in the GPS community and with other services?

DM: Don, we are scheduled to complete the transition and stand-up as the GPS Directorate on October 1, 2010. The Center is having one inactivation ceremony for all the Wings in SMC on September 8. The transition will be seamless and have a minimal effect on our military personnel. Our senior leadership is working on ensuring our materiel leader positions have group or squadron commander equivalency and will also be command-screened and boarded. There will not be very much difference within the Wing on a day-to-day basis. For the most part, the work, responsibility, and accountability will remain intact. The re-designation will have very little detriment upon the careers of the officers within the Wing. The officers' records will show a transition and re-designation to explain the change, and that it is no cause of their own. As far as future plans for the organization, the strength of the leadership here in the Wing will still be in place and will be just as effective as it is now to lead each individual in our organization and to move forward and progress in GPS capabilities into the next era. Other services will still look to us to continue to forge advancements in GPS satellites so that our influence in the world's GPS community will remain the standard: stronger than ever. Our organization will continue to acquire and sustain global navigation, positioning and timing services for our war fighters and civil users. We'll still be the Green Monsters everyone knows and loves!

DJ: What message would you like to leave with our readers as you move on from GPS to the milsatcom community?

DM: GPS is in great hands. I look forward to the challenges ahead.

DJ: Any final comments, Dave?

DM: It has truly been a pleasure leading the GPS Team — my best job in 30 years of service. And you, Don, have also been a welcome friend.

GPS improves the quality of life for everyone on the planet. It saves lives both on the battlefield and in our cities and towns across the globe. The U.S Air Force and Air Force Space Command have been the diligent stewards of GPS since program inception in the 1970s and continue its commitment to this critical component of our national infrastructure. The current GPS constellation has the most satellites and the greatest capability ever. We are committed to maintaining our current level of service, as well as striving to improve service and capability through ongoing modernization efforts. The Air Force will continue to pursue an achievable path maintaining GPS as the premier provider of positioning, navigation and timing for military and civilian users around the world.

DJ: Dave, everyone at GPS World wishes you the best of luck in your future endeavors, and thank you for your honesty and candid responses to our inquiries through the years. You were the leader the GPS Wing needed for the last three plus years and you have left a legacy of which you can be justly proud. And in my opinion if the GPS Wing, Directorate or JPO thinks they have seen the last of Dave Madden, they should think again. Best of luck in milsatcom.

http://www.gpsworld.com/gnss-system/gps-modernization/col-dave-madden-looks-back-and-forward-gps-future-10262<\/u><\/a>





Спасибо: 0 
ПрофильЦитата Ответить
moderator




Сообщение: 4487
Зарегистрирован: 09.02.08
Репутация: 0
ссылка на сообщение  Отправлено: 20.09.10 21:24. Заголовок: http://pnt.gov/publi..

Спасибо: 0 
ПрофильЦитата Ответить
Новых ответов нет , стр: 1 2 3 4 All [см. все]
Ответ:
1 2 3 4 5 6 7 8 9
видео с youtube.com картинка из интернета картинка с компьютера ссылка файл с компьютера русская клавиатура транслитератор  цитата  кавычки оффтопик свернутый текст

показывать это сообщение только модераторам
не делать ссылки активными
Имя, пароль:      зарегистрироваться    
Тему читают:
- участник сейчас на форуме
- участник вне форума
Все даты в формате GMT  3 час. Хитов сегодня: 41
Права: смайлы да, картинки да, шрифты нет, голосования нет
аватары да, автозамена ссылок вкл, премодерация откл, правка нет



Перспективная зенитная ракетная система противовоздушной и противоракетной обороны ЗРС С-400 "Триумф"