Robust Control for Spacecraft Rendezvous System with Thrust Saturation

被引：0

作者：

Wang, Qian ^{[1
]}

Xue, Anke ^{[1
]}

机构：

[1] Hangzhou Dianzi Univ, Inst Informat & Control, Hangzhou 310018, Peoples R China

来源：

PROCEEDINGS OF THE 28TH CHINESE CONTROL AND DECISION CONFERENCE (2016 CCDC) | 2016年

关键词：

Robust Gain Scheduling; Spacecraft Rendezvous; Parametric Riccati Equation; Thrust Saturation; Ellipsoid Sets; GAIN SCHEDULED CONTROL; LINEAR-SYSTEMS; GLOBAL STABILIZATION; ACTUATOR SATURATION; INPUT SATURATION; SUBJECT;

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：

The paper designed a robust nonlinear continuous static gain scheduling controller for the spacecraft rendezvous system with thrust saturation and parametric uncertainties by combining the parametric Riccati equation and the existing gain scheduling technique. By introducing the design parameter, the dynamic performance of the closed-loop system can be improved. In order to apply the proposed method, only need to solve a scalar nonlinear equation. The simulation results show the high dynamic performance and robustness of the designed controller.

引用

页码：2497 / 2502

页数：6

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