FAST THREE-AXIS ATTITUDE DETERMINATION USING VECTOR OBSERVATIONS AND INVERSE ITERATION.

被引：0
|
作者：
TIETZE, JOHN L.
机构：
来源：
| 1982年 / V 30卷 / N 2期
关键词：
COMPUTER PROGRAMS;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
AN ALGORITHM IS DEVELOPED TO FIND THE OPTIMAL ROTATION MATRIX THAT TRANSFORMS A SET OF REFERENCE VECTORS INTO A CORRESPONDING SET OF MEASUREMENT VECTORS. THE ALGORITHM MINIMIZES AQUADRATIC LOSS FUNCTION IN WHICH THE ROTATION MATRIX IS REPRESENTED AS A QUATERNION. THE MINIMIZING QUATERNION IS SHOWNTO BE AN EIGENVECTOR OF A SPECIAL MATRIX. THIS EIGENVECTOR IS FOUND BY INVERSE ITERATION. THE ALGORITHM IS COMPUTATIONALLY EFFICIENT AND ELIMINATES A SINGULARITY CONDITION CONTAINED IN A PREDECESSOR ALGORITHM.
引用
收藏
页码：171 / 179
相关论文
共 50 条
  • [41] Comparison of Feedback Three-Axis Magnetic Attitude Control Strategies
    Roldugin, Dmitry
    Okhitina, Anna
    Monakhova, Uliana
    Ovchinnikov, Mikhail
    Modenini, Dario
    AEROSPACE, 2023, 10 (12)
  • [42] TILTED WHEEL FOR THREE-AXIS ATTITUDE CONTROL OF A RIGID SATELLITE
    Inumoh, Lawrence O.
    Horri, Nadjim
    Pechev, Alex
    FIRST IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2012, PTS I AND II, 2012, 145 : 289 - 300
  • [43] Optimal attitude control for three-axis stabilized flexible spacecraft
    Zheng, JH
    Banks, SP
    Alleyne, H
    ACTA ASTRONAUTICA, 2005, 56 (05) : 519 - 528
  • [44] Three-axis active magnetic attitude control asymptotical study
    Ovchinnikov, M. Yu.
    Roldugin, D. S.
    Penkov, V. I.
    ACTA ASTRONAUTICA, 2015, 110 : 279 - 286
  • [45] Three-axis Magnetic Attitude Control by Delayed Output Feedback
    Xu, Chuanchuan
    Luo, Weiwei
    Yang, Xuefei
    2017 CHINESE AUTOMATION CONGRESS (CAC), 2017, : 3544 - 3549
  • [46] Integrated Attitude and Orbit Model of an Earth Orbiting Satellite Using Three-axis Control
    Mehrjardi, Mohamad Fakhari
    Sanusi, Hilmi
    Ali, Mohd. Alauddin Mohd.
    2015 INTERNATIONAL CONFERENCE ON SPACE SCIENCE AND COMMUNICATION (ICONSPACE), 2015, : 414 - 417
  • [47] Three-Axis Attitude Control Using Redundant Reaction Wheels with Continuous Momentum Dumping
    Hogan, Erik A.
    Schaub, Hanspeter
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (10) : 1865 - 1871
  • [48] Three-axis attitude control using combined gravity-gradient and solar pressure
    Circi, C.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2007, 221 (G1) : 85 - 90
  • [49] THREE-AXIS ATTITUDE CONTROL USING REDUNDANT REACTION WHEELS WITH CONTINUOUS MOMENTUM DUMPING
    Hogan, Erik A.
    Schaub, Hanspeter
    SPACEFLIGHT MECHANICS 2013, PTS I-IV, 2013, 148 : 1355 - 1367
  • [50] PD Controller for Three-Axis Satellite Attitude Control Using Discrete Kalman Filter
    Mehrjardi, Mohamad Fakhari
    Sanusi, Hilmi
    Ali, Mohd Alauddin Mohd
    Taher, Montadar Abas
    2014 INTERNATIONAL CONFERENCE ON COMPUTER, COMMUNICATIONS, AND CONTROL TECHNOLOGY (I4CT), 2014, : 83 - 85
12345