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
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