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Volumn , Issue , 2001, Pages

Sensitivity of initial state error covariance matrix in a practical adaptive EKF

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894496502     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (2)

References (10)
  • 1
    • 0029696291 scopus 로고    scopus 로고
    • Evolution of Flight Vehicles System Identification
    • Hammel P G & Jategaokar R V:."Evolution of Flight Vehicles System Identification." Journal of Aircraft, Vol, 33, No 1, pp 9-28 (1996).
    • (1996) Journal of Aircraft , vol.33 , Issue.1 , pp. 9-28
    • Hammel, P.G.1    Jategaokar, R.V.2
  • 5
    • 0024641201 scopus 로고
    • Dynamic Model for Real Time Estimation of Aerodynamic Characteristics
    • Jiang Quaneverfe, Chen Quiong Kang: "Dynamic Model for Real Time Estimation of Aerodynamic Characteristics." Journal of Aircraft, Vol-26, Bo 4, pp 315-321 (1986).
    • (1986) Journal of Aircraft , vol.26 , Issue.4 , pp. 315-321
    • Quaneverfe, J.1    Kang, C.Q.2
  • 9
    • 0016990568 scopus 로고
    • Adaptive Sequential Estimation with Unknown Noise Statistics
    • Myers K A and Eapley B D: "Adaptive Sequential Estimation with Unknown Noise Statistics." IEEE Transactions on Automatic Control, Vol. Ac 21, pp 520-525 (1976).
    • (1976) IEEE Transactions On Automatic Control , vol.Ac 21 , pp. 520-525
    • Myers, K.A.1    Eapley, B.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.