Robust attitude control for rapid multi-target tracking in spacecraft formation flying

A robust attitude tracking control scheme for spacecraft formation flying is presented. The leader spacecraft with a rapid mobile antenna and a camera is modeled. While the camera is tracking the ground target, the antenna is tracking the follower spacecraft. By an angular velocity constraint and an...

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Published in:Applied mathematics and mechanics 2008-02, Vol.29 (2), p.185-198
Main Author: 袁长清 李俊峰 王天舒 宝音贺西
Format: Article
Language:English
Subjects:
Angular velocity
Antennas
Applications of Mathematics
Cameras
Classical Mechanics
Fluid- and Aerodynamics
Formation flying
Mathematical Modeling and Industrial Mathematics
Mathematical models
Mathematics
Mathematics and Statistics
Partial Differential Equations
Spacecraft
Systems stability
Tracking
姿势控制
宇宙飞行
航天器
飞行力学
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cited_by cdi_FETCH-LOGICAL-c382t-3dade7060942bf08b4ea90b42bf1fec4addd42fab0acec25db0acb89e52f96813
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container_title Applied mathematics and mechanics
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creator 袁长清 李俊峰 王天舒 宝音贺西
description A robust attitude tracking control scheme for spacecraft formation flying is presented. The leader spacecraft with a rapid mobile antenna and a camera is modeled. While the camera is tracking the ground target, the antenna is tracking the follower spacecraft. By an angular velocity constraint and an angular constraint, two methods are proposed to compute the reference attitude profiles of the camera and antenna, respectively. To simplify the control design problem, this paper first derives the desired inverse system （DIS）, which can convert the attitude tracking problem of 3D space into the regulator problem. Based on DIS and sliding mode control （SMC）, a robust attitude tracking controller is developed in the presence of mass parameter uncertainties and external disturbance. By Lyapunov stability theory, the closed loop system stability can be achieved. The numerical simulations show that the proposed robust control scheme exhibits significant advantages for the multi-target attitude tracking of a two-spacecraft formation.
doi_str_mv 10.1007/s10483-008-0206-z
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1573-2754
language eng
recordid cdi_wanfang_journals_yysxhlx_e200802006
source Springer Nature
subjects Angular velocity
Antennas
Applications of Mathematics
Cameras
Classical Mechanics
Fluid- and Aerodynamics
Formation flying
Mathematical Modeling and Industrial Mathematics
Mathematical models
Mathematics
Mathematics and Statistics
Partial Differential Equations
Spacecraft
Systems stability
Tracking
姿势控制
宇宙飞行
航天器
飞行力学
title Robust attitude control for rapid multi-target tracking in spacecraft formation flying
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