A vacuum adaptive iterative guidance method of launch vehicle based on optimal analytical solution

被引：0
|
作者：
Department of Astronautics Engineering, Harbin Institute of Technology, Harbin 150001, China [1 ]
不详 [2 ]
机构：
来源：
Hangkong Xuebao | / 9卷 / 1696-1704期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Launch vehicles
引用
收藏
相关论文
共 50 条
  • [21] Ascent Guidance for Launch Vehicle Based on Receding Horizon Control
    He, Qianwei
    Yang, Ye
    Liu, Lei
    Cheng, Zhongtao
    PROCEEDINGS OF THE 39TH CHINESE CONTROL CONFERENCE, 2020, : 3391 - 3396
  • [22] Simulation of Guidance Subsystem of Launch Vehicle Based on Matlab/Simulink
    Lin, Lan
    Li, Hui
    Ding, Wei
    2009 WASE INTERNATIONAL CONFERENCE ON INFORMATION ENGINEERING, ICIE 2009, VOL I, 2009, : 439 - +
  • [23] ANALYTICAL SOLUTION OF OPTIMAL TRAJECTORY-SHAPING GUIDANCE
    RAO, MN
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1989, 12 (04) : 600 - 601
  • [24] ANALYTICAL SOLUTION OF OPTIMAL TRAJECTORY-SHAPING GUIDANCE
    LIN, CF
    TSAI, LL
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1987, 10 (01) : 61 - 66
  • [25] Guidance and control of a launch vehicle using a stochastic gradient projection method
    Madeira, F
    Rios-Neto, A
    AUTOMATICA, 2000, 36 (03) : 427 - 438
  • [26] OPTIMAL EXPLICIT GUIDANCE OF MULTISTAGE LAUNCH VEHICLE ALONG 3-DIMENSIONAL TRAJECTORY
    SINHA, SK
    SHRIVASTAVA, SK
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1990, 13 (03) : 394 - 403
  • [27] Adaptive integrated guidance and control for air-breathing phase of reusable launch vehicle
    Radhakrishnan, Rani
    Hari, Priyadarshnam
    Simha, M. S. Harsha
    Sivan, K.
    INTERNATIONAL JOURNAL OF DYNAMICS AND CONTROL, 2024, 12 (11) : 4020 - 4033
  • [28] Optimal explicit guidance of multistage launch vehicle along three-dimensional trajectory
    Sinha, S.K., 1600,
  • [29] Analysis of Fault Modes and Applications of Self-Adaptive Guidance Technology for Launch Vehicle
    Chang W.-Q.
    Zhang Z.-G.
    Yuhang Xuebao/Journal of Astronautics, 2019, 40 (03): : 302 - 309
  • [30] Cooperative Reentry Guidance for Intelligent Lateral Maneuver of Hypersonic Vehicle Based on Downrange Analytical Solution
    Zhang W.
    Yu W.
    Li J.
    Chen W.
    Binggong Xuebao/Acta Armamentarii, 2021, 42 (07): : 1400 - 1411
12345