Controllability analysis and attitude path planning of underactuated spacecraft systems

被引：10

作者：

Zhang, Jiawei ^{[1
]}

Ma, Kemao ^{[1
]}

Meng, Guizhi ^{[1
]}

机构：

[1] Harbin Inst Technol, Control & Simulat Ctr, Harbin 150006, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2014年 / 33卷 / 01期

关键词：

Flywheel; Underactuated spacecraft; Gauss pseudospectral method; Controllability; Path planning; PSEUDOSPECTRAL METHODS; STABILIZATION;

D O I：

10.1016/j.ast.2014.01.003

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The controllability analysis and attitude path planning are addressed for an underactuated spacecraft using two flywheels as actuators. Considering the spacecraft and flywheels as a whole system, we describe the dynamics of the system on an angular momentum level set such that the system is controllable with arbitrary initial momentum and direction of the torque singular vector. Moreover, an optimal performance index is proposed with the influence of friction torques in flywheels considered. With this index being optimized, Gauss Pseudospectral Method (GPM) is used to design the attitude path of the system, which satisfies the spacecraft maneuver requirement. Finally, simulation results show the effectiveness of the attitude path planning method. Crown Copyright (C) 2014 Published by Elsevier Masson SAS. All rights reserved.

引用

页码：76 / 81

页数：6

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