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Volumn , Issue , 2000, Pages

Error dynamics of model based INS/GPS navigation for an autonomously flying helicopter

Author keywords

Augmented navigation system; Autonomous and unmanned vehicles; INS GPS error propagation; Model based navigation; Navigation error modeling; Strapdown inertial navigation

Indexed keywords

ERROR ANALYSIS; INERTIAL NAVIGATION SYSTEMS; UNMANNED VEHICLES;

EID: 85088183994     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4465     Document Type: Conference Paper
Times cited : (10)

References (13)
  • 1
    • 0024001174 scopus 로고
    • Control theoretic approach to inertial navigation systems
    • Bar-Itzhack, I.Y. and N. Berman (1988). Control theoretic approach to inertial navigation systems. Guidance, Control, and Dynamics 11 (3), 237-245.
    • (1988) Guidance, Control, and Dynamics , vol.11 , Issue.3 , pp. 237-245
    • Bar-Itzhack, I.Y.1    Berman, N.2
  • 8
    • 6344259345 scopus 로고
    • Geodetic positioning by inertial and satellite systems: An overview
    • ed. K. Linkwitz, and U. Hangleiter.Springer
    • Grafarend, Erik W. (1989). Geodetic positioning by inertial and satellite systems: An overview. In: High Precision Navigation: ed. K. Linkwitz, and U. Hangleiter. pp. 34-73. Springer.
    • (1989) High Precision Navigation , pp. 34-73
    • Grafarend, E.W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.