Real-time optimal state feedback control for tethered subsatellite system

被引：3
|
作者：
Kokubun, K [1 ]
Anazawa, S [1 ]
Fujii, HA [1 ]
机构：
[1] TOKYO METROPOLITAN INST TECHNOL, DEPT AEROSP ENGN, TOKYO 191, JAPAN
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1996年 / 19卷 / 04期
关键词：
D O I：
10.2514/3.21728
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In the present work, real-time state feedback control is applied successfully to a control problem of the tethered subsatellite system. The stabilized continuation method converts the two-point boundary-value problem into the initial-value problem, and the optimal state feedback controller is derived from the receding horizon control method. Results of numerical simulation show that the subsatellite is well controlled for the terminal state during deployment and retrieval phases.
引用
收藏
页码：972 / 974
页数：3
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