Quaternion-Based Hybrid Control for Robust Global Attitude Tracking

被引:292
|
作者
Mayhew, Christopher G. [1 ]
Sanfelice, Ricardo G. [2 ]
Teel, Andrew R. [3 ]
机构
[1] Robert Bosch Res & Technol Ctr, Palo Alto, CA 94304 USA
[2] Univ Arizona, Dept Aerosp & Mech Engn, Tucson, AZ 85721 USA
[3] Univ Calif Santa Barbara, Ctr Control Dynam Syst & Computat, Dept Elect & Comp Engn, Santa Barbara, CA 93106 USA
基金
美国国家科学基金会;
关键词
Attitude control; hybrid control; output feedback; robustness; spacecraft; RIGID-BODY; STABILIZATION; FEEDBACK; REJECTION; OBSERVER; DYNAMICS;
D O I
10.1109/TAC.2011.2108490
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
It is well known that controlling the attitude of a rigid body is subject to topological constraints. We illustrate, with examples, the problems that arise when using continuous and (memoryless) discontinuous quaternion-based state-feedback control laws for global attitude stabilization. We propose a quaternion-based hybrid feedback scheme that solves the global attitude tracking problem in three scenarios: full state measurements, only measurements of attitude, and measurements of attitude with angular velocity measurements corrupted by a constant bias. In each case, the hybrid feedback is dynamic and incorporates hysteresis-based switching using a single binary logic variable for each quaternion error state. When only attitude measurements are available or the angular rate is corrupted by a constant bias, the proposed controller is observer-based and incorporates an additional quaternion filter and bias observer. The hysteresis mechanism enables the proposed scheme to simultaneously avoid the "unwinding phenomenon" and sensitivity to arbitrarily small measurement noise that is present in discontinuous feedbacks. These properties are shown using a general framework for hybrid systems, and the results are demonstrated by simulation.
引用
收藏
页码:2555 / 2566
页数:12
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