AN ATTITUDE CONTROL SYSTEM FOR LARGE LAUNCH VEHICLES

被引:1
|
作者
SELTZER, SM
机构
关键词
D O I
10.2514/3.29653
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:748 / +
页数:1
相关论文
共 50 条
  • [1] Attitude control technology of new-generation launch vehicles
    Wu, Yansheng
    He, Linshu
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2009, 35 (11): : 1294 - 1297
  • [2] Optimal Soft Landing Guidance and Attitude Control for Reusable Launch Vehicles
    Jeon, Ho-Young
    Cho, Jun-Hyon
    Kim, Jong-Han
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2022, 50 (04) : 251 - 257
  • [3] AN ATTITUDE CONTROL SYSTEM FOR SPACE VEHICLES
    HAEUSSERMANN, W
    ARS JOURNAL, 1959, 29 (03): : 203 - 207
  • [4] Study on simulation of launch vehicle attitude control system
    Li, Hui
    Jing, Xiaogang
    Zhuang, Wanyu
    2005 IEEE International Conference on Mechatronics and Automations, Vols 1-4, Conference Proceedings, 2005, : 2022 - 2025
  • [5] NONLINEAR ANALYSIS OF A LAUNCH VEHICLE ATTITUDE CONTROL SYSTEM
    SELTZER, SM
    JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (03) : 366 - &
  • [6] Strategy on Multi-Rate Gyroscopes Application to Attitude Control of Launch Vehicles
    Wang J.-M.
    Zhang D.-M.
    Hong L.-Y.
    Li N.
    Yuhang Xuebao/Journal of Astronautics, 2020, 41 (03): : 337 - 342
  • [7] SATURN LAUNCH VEHICLES NAVIGATION GUIDANCE, AND CONTROL SYSTEM
    HAEUSSER.W
    AUTOMATICA, 1971, 7 (05) : 537 - &
  • [8] Research on application of PXI technology in test launch and control system for launch vehicles
    Li Yan
    Cai Yuanwen
    Cheng Long
    ISTM/2007: 7TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-7, CONFERENCE PROCEEDINGS, 2007, : 40 - 44
  • [9] Attitude control design for reusable launch vehicles using adaptive fuzzy control with compensation controller
    Mao, Qi
    Dou, Liqian
    Zong, Qun
    Ding, Zhengtao
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (03) : 823 - 836
  • [10] ADP-based intelligent attitude fault-tolerant control for launch vehicles
    Liang X.
    Hu C.
    Zhou Z.
    Wang Q.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2021, 42 (04):