Switching Angular Velocity Observer for Rigid-Body Attitude Stabilization and Tracking Control

被引:42
作者
Chunodkar, Apurva A. [1 ]
Akella, Maruthi R. [1 ]
机构
[1] Univ Texas Austin, Dept Aerosp Engn & Engn Mech, Austin, TX 78712 USA
关键词
OUTPUT-FEEDBACK; MOTION;
D O I
10.2514/1.60998
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper provides a new switching angular velocity observer formulation to the classical problem of rigid-body attitude tracking control in the absence of angular rate measurements. Exponential convergence of the angular velocity state estimation errors is proven using a novel error signal definition through the use of this switching-type observer. The observer synthesis and convergence properties are independent of controller design. The switching ensures C-0 continuity for all the estimated states. Further, the maximum number of switches required by the observer is shown to be finite and that zeno-type behavior cannot occur. A "separation-property" type result for the attitude tracking problem is established, wherein a proportional-derivative controller uses angular velocity estimates from the proposed switching observer in the absence of actual angular rate measurements, while ensuring almost global asymptotic stability for the overall closed-loop tracking error dynamics. The separation property is also proven to hold when a gyroscopic nonlinear compensation term is added to the proportional-derivative controller.
引用
收藏
页码:869 / 878
页数:10
相关论文
共 17 条
[1]   Rigid body attitude tracking without angular velocity feedback [J].
Akella, M.R. .
Systems and Control Letters, 2001, 42 (04) :321-326
[2]   A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon [J].
Bhat, SP ;
Bernstein, DS .
SYSTEMS & CONTROL LETTERS, 2000, 39 (01) :63-70
[3]   Output feedback control for attitude tracking [J].
Caccavale, F ;
Villani, L .
SYSTEMS & CONTROL LETTERS, 1999, 38 (02) :91-98
[4]   Quaternion-based adaptive attitude tracking controller without velocity measurements [J].
Costic, BT ;
Dawson, DM ;
Kapila, V .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2001, 24 (06) :1214-1222
[5]   Minimum model error approach for attitude estimation [J].
Crassidis, JL ;
Markley, FL .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (06) :1241-1247
[6]  
Ioannou P.A., 1996, Robust Adaptive Control, P76
[7]   Attitude regulation about a fixed rotation axis [J].
Lawton, J ;
Beard, RW .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (02) :253-258
[8]   Attitude control without angular velocity measurement: A passivity approach [J].
Lizarralde, F ;
Wen, JT .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1996, 41 (03) :468-472
[9]  
Nicosia S., 1992, IEEE T AERO ELEC SYS, V28, P973
[10]   A GLOBALLY CONVERGENT ANGULAR VELOCITY OBSERVER FOR RIGID BODY MOTION [J].
SALCUDEAN, S .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1991, 36 (12) :1493-1497