MODEL PREDICTIVE CONTROL OF SPACECRAFT RELATIVE MOTION MANEUVERS USING THE IPA-SQP APPROACH

被引：0

作者：

Park, Hyeongjun ^{[1
]}

Kolmanovsky, Ilya ^{[1
]}

Sun, Jing ^{[2
]}

机构：

[1] Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA

[2] Univ Michigan, Dept Elect Engn & Comp Sci, Dept Naval Architecture & Marine Engn, Ann Arbor, MI 48109 USA

来源：

PROCEEDINGS OF THE ASME 2013 DYNAMIC SYSTEMS AND CONTROL CONFERENCE (DSCC2013), VOL. 1 | 2013年

关键词：

GUIDANCE;

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：

In this paper, a Model Predictive Controller (MPC) based on the Integrated Perturbation Analysis and Sequential Quadratic Programming (IPA-SQP) is designed and analyzed for spacecraft relative motion maneuvering. To evaluate the effectiveness of the IPA-SQP MPC, the results are compared with the linear quadratic MPC algorithm developed in [4, 13-15]. It is shown that the IPA-SQP algorithm can handle directly nonlinear constraints on thrust magnitude without resorting to saturation or polyhedral norm approximations. Spacecraft fuel consumption related metrics are examined for performance evaluation and comparison.

引用

页数：9

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