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航天器姿态预设性能控制方法综述
引用本文:魏才盛,罗建军,殷泽阳.航天器姿态预设性能控制方法综述[J].宇航学报,2019,40(10):1167-1176.
作者姓名:魏才盛  罗建军  殷泽阳
作者单位:西北工业大学航天学院航天飞行动力学技术重点实验室,西安 710072
基金项目:国家自然科学基金重大项目(61690210, 61690211)
摘    要:针对存在不确定惯量矩阵及其它未知不确定性(如执行器故障、航天器结构发生突变等)下的航天器姿态控制问题,综述了预设性能控制及其应用的研究进展。首先阐释了预设性能控制方法的基本内涵及其关键步骤;然后分析总结了现有航天器姿态控制以及预设性能控制研究的基本概况与发展趋势;最后面向未来复杂化、智能化的空间任务对航天器控制系统提出的新需求,提出航天器预设性能控制值得研究的问题和方向。

关 键 词:预设性能控制  航天器姿态  鲁棒控制  瞬态与稳态性能  
收稿时间:2019-06-15

A Review of Prescribed Performance Control for Spacecraft Attitude
WEI Cai sheng,LUO Jian jun,YIN Ze yang.A Review of Prescribed Performance Control for Spacecraft Attitude[J].Journal of Astronautics,2019,40(10):1167-1176.
Authors:WEI Cai sheng  LUO Jian jun  YIN Ze yang
Affiliation:National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China
Abstract:For the spacecraft attitude control problem in the presence of uncertain inertial matrix and other unknown uncertainties such as actuator faults and change of spacecraft structures, a fully comprehensive review of the prescribed performance control (PPC) methodology is investigated in this paper. In this review, the basic explanation of PPC is given along with an introduction for its three key steps. Then, the current development of the attitude control methods and PPC method is analyzed and discussed. Finally, faced with the requirements raised by the future complicated and intelligent space missions, some open issues and research suggestions on PPC in aerospace applications are presented.
Keywords:Prescribed performance control  Spacecraft attitude  Robust control  Transient and steady-state performance  
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