An Adaptive Tracking Control Method for Braking Phase of Lunar Soft Landing

被引：0
|
作者：
Han, Yu [1 ]
Fan, Wei [2 ]
Cheng, Hao [3 ]
Zheng, Bo [1 ]
Zhang, Xianliang [1 ]
机构：
[1] Shanghai Aerosp Control Technol Inst, Shanghai Key Lab Space Intelligent Control Techno, Shanghai, Peoples R China
[2] Shanghai Inst Satellite Engn, Shanghai, Peoples R China
[3] Shanghai Aerosp Control Technol Inst, Shanghai, Peoples R China
来源：
2020 CHINESE AUTOMATION CONGRESS (CAC 2020) | 2020年
基金：
国家重点研发计划;
关键词：
adaptive control; attitude tracking control; lunar soft landing; braking phase;
D O I：
10.1109/CAC51589.2020.9327840
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
During braking phase of lunar soft landing, the high-thrust orbit-control engine works at maximum thrust, the interference and interference-torque is in critical condition, and there is seriously attitude and orbit coupling situation. In this paper we address the problem of braking phase of lunar soft landing. An adaptive tracking control method based on traditional feedback control is designed to obtain that the control system works well under braking phase of lunar soft landing. Taking the parameters of the Apollo in the simulation model, a comparison between the traditional control method and the adaptive tracking control method is undertaken. It is shown that the proposed controller copes with braking phase and shows faster convergence speed and higher stability precision.
引用
收藏
页码：5573 / 5578
页数：6
相关论文
共 50 条
  • [1] An exact penalty function method for optimal lunar soft landing control problem
    Gao Xiangyu
    Shao Lili
    Liu Hao
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 2215 - 2220
  • [2] Neuro-Optimal Guidance Control for Lunar Soft Landing
    Wang Dayi(School of Astronautics
    JournalofSystemsEngineeringandElectronics, 1999, (03) : 22 - 31
  • [3] Optimization of lunar soft landing trajectory based on hybrid method
    Peng, Kun
    Guo, Linli
    Xiang, Kaiheng
    Wang, Ping
    Xu, Shijie
    Peng, K. (bhkpeng@126.com), 1600, Beijing University of Aeronautics and Astronautics (BUAA) (40): : 910 - 915
  • [4] Adaptive guidance and control of uncertain lunar landers in terminal landing phases
    Sun, Liang
    Sun, Guang
    Jiang, Jingjing
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2020, 142
  • [5] Trajectory optimization for lunar soft landing with a Hamiltonian-based adaptive mesh refinement strategy
    Ma, Lin
    Shao, Zhijiang
    Chen, Weifeng
    Song, Zhengyu
    ADVANCES IN ENGINEERING SOFTWARE, 2016, 100 : 266 - 276
  • [6] Applying Nonlinear programming to solve optimal control problem of lunar probe soft landing
    Shan Yongzheng
    Duan Guangren
    PROCEEDINGS OF THE 26TH CHINESE CONTROL CONFERENCE, VOL 6, 2007, : 485 - +
  • [7] Autonomous navigation and guidance for pinpoint lunar soft landing
    Huang, Xiangyu
    Wang, Dayi
    2007 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS, VOLS 1-5, 2007, : 1148 - 1153
  • [8] GNC system scheme for lunar soft landing spacecraft
    Wang, Dayi
    Huang, Xiangyu
    Guan, Yifeng
    ADVANCES IN SPACE RESEARCH, 2008, 42 (02) : 379 - 385
  • [9] Attitude Constrained Robust Explicit Guidance for Terminal Phase of Autonomous Lunar Soft-Landing
    Radhakant Padhi
    Avijit Banerjee
    P. S. V. S. Sai Kumar
    S. P. Parvathi
    The Journal of the Astronautical Sciences, 71
  • [10] Sequential Convex Optimization Method for Lunar Landing during Powered Descent Phase
    Deng Y.
    Mu R.
    Peng N.
    Wu P.
    Yuhang Xuebao/Journal of Astronautics, 2022, 43 (08): : 1029 - 1039
12345