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Volumn 13, Issue 4, 2004, Pages 369-372

Optimal observability analysis of gimbled inertial navigation system on the moving base

Author keywords

Condition number; Gimbled inertial navigation system (GINS); Observability; Singular value

Indexed keywords

ALIGNMENT; KALMAN FILTERING; OBSERVABILITY; STOCHASTIC CONTROL SYSTEMS;

EID: 13644273075     PISSN: 10040579     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (3)

References (5)
  • 2
    • 0036553926 scopus 로고    scopus 로고
    • Observability analysis of SINS' error states
    • Chinese source
    • Wu Meiping, Hu Xiaoping. Observability analysis of SINS' error states[J]. Journal of Astronautics, 2002,23(2):54-76.(in Chinese)
    • (2002) Journal of Astronautics , vol.23 , Issue.2 , pp. 54-76
    • Wu, M.1    Hu, X.2
  • 4
    • 2642543076 scopus 로고    scopus 로고
    • Research on multiposition alignment of SINS
    • Chinese source
    • Wang Yandong, Fan Yuezu. Research on multiposition alignment of SINS[J]. Journal of Chinese Inertial Technology, 2000,8(3):17-19. (in Chinese)
    • (2000) Journal of Chinese Inertial Technology , vol.8 , Issue.3 , pp. 17-19
    • Wang, Y.1    Fan, Y.2
  • 5
    • 0003469273 scopus 로고
    • Beijing: Aviation Industry Press, Chinese source
    • Yuan Xin, Yu Jixiang, Chen Zhe. Navigation system[M]. Beijing: Aviation Industry Press, 1993.30-69. (in Chinese)
    • (1993) Navigation System , pp. 30-69
    • Yuan, X.1    Yu, J.2    Chen, Z.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.