Robust Disturbance Rejection Guidance Law for Autonomous Rendezvous with Tumbling Non-Cooperative Spacecraft

被引：0
|
作者：
Ding, Yibo [1 ]
Guan, Yingzi [1 ]
Cui, Naigang [1 ]
Yang, Feng [1 ]
机构：
[1] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Heilongjiang, Peoples R China
来源：
2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2017年
关键词：
Rendezvous; Tumbling Non-Cooperative; Generalized Super-Twisting Algorithm; Homogeneous High Order Sliding Mode Observer; Disturbance Rejection; SLIDING MODE;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A robust disturbance rejection guidance law for autonomous rendezvous with non-cooperative target is studied using generalized super-twisting algorithm (GSTA) and homogeneous high order sliding mode observer (HHOSMO). The proposed method is able to ensure a service spacecraft subject to modeling uncertainties, external disturbances and actuator/thruster failures accomplishes the rendezvous mission without collision. Considering the restriction of Clohessy-Wiltshire (C-W) equations, a coupled relative motion model is established in line of sight coordinate frame. The GSTA is used as a robust continuous guidance law while the HHOSMO is able to observe and compensate the lumped disturbances in a finite time to enhance the ability of disturbance rejection. The stability of the closed-loop system is analyzed using Lyapunov stability criteria. Results obtained from numerical simulations demonstrate the validity of the method formulated in this paper.
引用
收藏
页码：5346 / 5351
页数：6
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