Quaternion-Based Bang-Bang Attitude Stabilizer for Rotating Rigid Bodies

被引：2
|
作者：
Serpelloni, Edoardo [1 ]
Maggiore, Manfredi [1 ]
Damaren, Christopher J. [2 ]
机构：
[1] Univ Toronto, Elect & Comp Engn Dept, Toronto, ON M5S 2J7, Canada
[2] Univ Toronto, Inst Aerosp Studies, Toronto, ON M5S 2J7, Canada
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2017年 / 40卷 / 06期
基金：
加拿大自然科学与工程研究理事会;
关键词：
OPTIMAL 3-AXIS REORIENTATION; ON-OFF THRUSTERS; FLEXIBLE SPACECRAFT; SYSTEMS; MANEUVERS; FEEDBACK; DESIGN;
D O I：
10.2514/1.G002271
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The hybrid feedback is modified so as to take full advantage of the quaternion parametrization of the spacecraft attitude. The controller achieves practical stabilization of the spacecraft attitude assuming the full nonlinear dynamics of the spacecraft, while avoiding chattering and high-frequency switching of the actuators. An extensive Monte Carlo numerical analysis indicates that the result might be global. the attitude controller is the first bang-bang feedback controller with guaranteed stability properties and guaranteed bounded switching frequency, even in the presence of measurement noise.
引用
收藏
页码：1523 / +
页数：7
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