DocumentCode
3185564
Title
Navigation systems integration
Author
Gordon, G.S.
Author_Institution
GEC Marconi Navigation & Electron-Opt. Syst., Edinburgh, UK
fYear
1998
fDate
35836
Firstpage
42461
Lastpage
416
Abstract
Principles of integrated navigation and optimal estimation theory are discussed. The complexity of navigation system requirements is described, and a comprehensive system design approach is presented. The paper concludes by looking at specific issues which arise in testing integrated navigation systems. The paper is biased towards military vehicle navigation. However the potential for application in commercial vehicles will be evident.
Keywords
aircraft navigation; Kalman filter; airborne navigation systems; combined INS/GPS; comprehensive system design approach; covariance matrix; hardware/software in the loop testing; integrated navigation; military vehicle navigation; mission profiles; multiple sensors; navigation systems integration; optimal estimation theory; predictor-corrector algorithm; simulator system; state vector model; synergy; system requirements complexity; testing issues; truth model;
fLanguage
English
Publisher
iet
Conference_Titel
Airborne Navigation Systems Workshop (Ref. No. 1998/275), IEE
Type
conf
DOI
10.1049/ic:19980390
Filename
689574
Link To Document