Q-Method Extended Kalman Filter

被引：33
作者：
Ainscough, Thomas [1 ]
Zanetti, Renato [1 ,2 ]
Christian, John [3 ]
Spanos, Pol D. [4 ]
机构：
[1] Rice Univ, US Air Force, Charles Stark Draper Lab, Houston, TX 77058 USA
[2] Charles Stark Draper Lab, Houston, TX 77058 USA
[3] W Virginia Univ, Dept Mech & Aerosp Engn, Morgantown, WV 26508 USA
[4] Rice Univ, Ryon Chair Engn, Houston, TX 77005 USA
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2015年 / 38卷 / 04期
关键词：
ATTITUDE-DETERMINATION; SPACECRAFT ATTITUDE; VECTOR OBSERVATIONS; QUATERNION ESTIMATION; ALGORITHM; REQUEST; QUEST;
D O I：
10.2514/1.G000118
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A new algorithm is proposed that smoothly incorporates the nonlinear estimation of the attitude quaternion using Davenport's q-method and the estimation of nonattitude states through an extended Kalman filter. The new algorithm is compared to an existing one and the various similarities and differences are discussed. The validity of the proposed approach is confirmed by numerical simulations.
引用
收藏
页码：752 / 760
页数：9
相关论文
共 24 条
  • [1] [Anonymous], 1977, Technical Report CSC/TM-77/6034
  • [2] ATTITUDE DETERMINATION FROM VECTOR OBSERVATIONS - QUATERNION ESTIMATION
    BARITZHACK, IY
    OSHMAN, Y
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1985, 21 (01) : 128 - 136
  • [3] REQUEST: A recursive QUEST algorithm for sequential attitude determination
    BarItzhack, IY
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (05) : 1034 - 1038
  • [4] Bucy R. S., 2005, Filtering for Stochastic Processing with Applications to Guidance, V2nd, P55
  • [5] Optimal-REQUEST algorithm for attitude determination
    Choukroun, D
    Bar-Itzhack, IY
    Oshman, Y
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2004, 27 (03) : 418 - 425
  • [6] Sequential Optimal Attitude Recursion Filter
    Christian, John A.
    Lightsey, E. Glenn
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (06) : 1787 - 1800
  • [7] Farrenkopf R.L., 1978, J GUID CONTROL DYNAM, V1, P282, DOI DOI 10.2514/3.55779
  • [8] Gelb A., 1996, APPL OPTIMAL ESTIMAT, p[190, 182]
  • [9] KALMAN FILTERING FOR SPACECRAFT ATTITUDE ESTIMATION
    LEFFERTS, EJ
    MARKLEY, FL
    SHUSTER, MD
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1982, 5 (05) : 417 - 429
  • [10] Averaging quaternions
    Markley, F. Landis
    Oshman, Yaakov
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (04) : 1193 - 1197
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