Control law synthesis for large flexible spacecraft

被引：0
|
作者：
van, Woerkom, P.Th.L.M.
机构：
来源：
Nationaal Lucht-en Ruimtevaartlaboratorium, Verslagen en Verhandelingen | 1991年 / TP 91155期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [1] SYNTHESIS AND SURVEY OF CONTROL LAWS FOR LARGE FLEXIBLE SPACECRAFT
    VANWOERKOM, PTLM
    CONTROL-THEORY AND ADVANCED TECHNOLOGY, 1993, 9 (03): : 639 - 669
  • [2] IDENTIFICATION AND CONTROL OF LARGE FLEXIBLE SPACECRAFT
    HARRIS, S
    KAKAD, YP
    PROCEEDINGS : THE TWENTY-FIRST SOUTHEASTERN SYMPOSIUM ON SYSTEM THEORY, 1989, : 284 - 288
  • [3] CONTROL OF SPINNING FLEXIBLE SPACECRAFT BY MODAL SYNTHESIS
    MEIROVITCH, L
    VANLANDINGHAM, HF
    OZ, H
    ACTA ASTRONAUTICA, 1977, 4 (9-10) : 985 - 1010
  • [4] Dynamic modeling and control of large flexible spacecraft combination
    Zhou ZhiCheng
    Wang XingLong
    Qu GuangJi
    SCIENTIA SINICA-PHYSICA MECHANICA & ASTRONOMICA, 2019, 49 (02)
  • [5] Design of a large angle maneuvering control law for spacecraft
    Beijing Astronautics Control Center, Beijing 100094, China
    Yuhang Xuebao, 2006, 6 (1223-1227):
  • [6] PULSE-MODULATED CONTROL SYNTHESIS FOR A FLEXIBLE SPACECRAFT
    ANTHONY, TC
    WIE, B
    CARROLL, S
    AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS, 1989, : 65 - 76
  • [7] PULSE-MODULATED CONTROL SYNTHESIS FOR A FLEXIBLE SPACECRAFT
    ANTHONY, TC
    WIE, B
    CARROLL, S
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1990, 13 (06) : 1014 - 1022
  • [8] Control of flexible spacecraft using dynamic inversion and μ-synthesis
    Malekzadeh, M.
    Naghash, A.
    Talebi, H. A.
    JOURNAL OF VIBRATION AND CONTROL, 2011, 17 (13) : 1938 - 1951
  • [9] Attitude tracking control of flexible spacecraft with large amplitude slosh
    Mingle Deng
    Baozeng Yue
    Acta Mechanica Sinica, 2017, (06) : 1095 - 1102
  • [10] Robust Model Predictive Attitude Control of Large Flexible Spacecraft
    Guan P.
    Wu X.-Y.
    Ge X.-S.
    Cao Y.-T.
    Yuhang Xuebao/Journal of Astronautics, 2022, 43 (04): : 476 - 485
12345