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航天器近距离相对运动的鲁棒约束模型预测控制

朱彦伟 杨乐平

控制理论与应用2009,Vol.26Issue(11):1273-1276,1281,5.
控制理论与应用2009,Vol.26Issue(11):1273-1276,1281,5.

航天器近距离相对运动的鲁棒约束模型预测控制

Spacecraft proximity relative motion under robust constrained model predictive control

朱彦伟 1杨乐平1

作者信息

  • 1. 国防科技大学航天与材料工程学院,湖南长沙,410073
  • 折叠

摘要

Abstract

With the development of on-orbit service, there is an increasing desire to control spacecraft proximity op-erations precisely. By employing the set theory, the mixed-integer linear programming(MILP) and the variable horizon model predictive control(MPC), we solve the robust control problem of spacecraft proximity operations, considering con-trol constraints, state constraints, unknown bounded disturbance, control error and navigation error. Firstly, the finite-time maneuvering with a predetermined target set is formulated by the discrete C-W dynamics, the time-fuel cost function and the linear constraints. Secondly, the robust variable horizon MPC algorithm is introduced to ensure the robust feasibility and the finite-time entry of the target set. The feasibility is analyzed by using the i-step robust controllable set. The navi-gation error is treated as a bounded disturbance by set operations. The controller is implemented using MILP optimization. Finally, the simulation results show that the controller is efficient and robust.

关键词

航天器/相对运动/约束压缩/模型预测控制/混合整数线性规划

Key words

spacecraft/ relative motion/ constraint tightening/ MPC/ MILP

分类

航空航天

引用本文复制引用

朱彦伟,杨乐平..航天器近距离相对运动的鲁棒约束模型预测控制[J].控制理论与应用,2009,26(11):1273-1276,1281,5.

基金项目

国家"863"计划资助项目(2007AA704114). (2007AA704114)

控制理论与应用

OA北大核心CSCDCSTPCD

1000-8152

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