Observer-Based Adaptive Spacecraft Attitude Control With Guaranteed Performance Bounds

被引：33
|
作者：
de Ruiter, Anton H. J. [1 ]
机构：
[1] Ryerson Univ, Dept Aerosp Engn, Toronto, ON M5B 2K3, Canada
来源：
IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 2016年 / 61卷 / 10期
关键词：
Attitude control; attitude observer; ultimate boundedness; SINGLE VECTOR MEASUREMENT; TRACKING CONTROL; GYRO NOISE;
D O I：
10.1109/TAC.2015.2503719
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This technical note considers observer-based adaptive attitude tracking of fully actuated spacecraft with known bounds on the disturbance torques acting on the spacecraft. Given any attitude and angular velocity observer with known ultimate bounds on the estimation errors, sequences of successively less conservative ultimate bounds on the attitude and angular velocity tracking errors are obtained.
引用
收藏
页码：3146 / 3151
页数：6
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