Design of reliable control systems possessing actuator redundancies

被引：45

作者：

Jiang, J ^{[1
]}

Zhao, Q

机构：

[1] Univ Western Ontario, Dept Elect & Comp Engn, London, ON N6A 5B9, Canada

[2] Univ Manitoba, Dept Elect & Comp Engn, Winnipeg, MB R3T 5V6, Canada

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2000年 / 23卷 / 04期

关键词：

D O I：

10.2514/2.4587

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The explicit definitions of actuator redundancies are introduced. A design scheme is then presented to synthesize reliable control against actuator failures for dynamic systems possessing actuator redundancies. The properly designed controller is able to guarantee the stability and to maintain the steady-state tracking performance in the event of actuator failures. The design method is based on a robust regional eigenvalue assignment technique with the help of a precompensator. The effectiveness of the proposed method has been verified using an example of the aircraft bank angle control problem.

引用

页码：709 / 718

页数：10

共 30 条

[1]

Ackermann J., 1985, SAMPLED DATA CONTROL

[2]

Ackermann J., 1993, Robust Control: Systems with Uncertain Physical Parameters

[3] A SURVEY OF EXTREME POINT RESULTS FOR ROBUSTNESS OF CONTROL-SYSTEMS [J].

BARMISH, BR ;

KANG, HI .

AUTOMATICA, 1993, 29 (01) :13-35

[4] Reliable decentralized stabilization of linear systems [J].

Gündes, AN .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1998, 43 (12) :1733-1739

[5] RESTRUCTURABLE CONTROL USING PROPORTIONAL-INTEGRAL IMPLICIT MODEL FOLLOWING [J].

HUANG, CY ;

STENGEL, RF .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1990, 13 (02) :303-309

[6] DESIGN OF RECONFIGURABLE CONTROL-SYSTEMS USING EIGENSTRUCTURE ASSIGNMENTS [J].

JIANG, J .

INTERNATIONAL JOURNAL OF CONTROL, 1994, 59 (02) :395-410

[7]

MacFarlane A. G. J., 1980, Complex Variable Methods for Linear Multivariable Feedback Systems

[8] DETECTION DELAYS, FALSE ALARM RATES AND THE RECONFIGURATION OF CONTROL-SYSTEMS [J].

MARITON, M .

INTERNATIONAL JOURNAL OF CONTROL, 1989, 49 (03) :981-992

[9] NEW TECHNIQUE FOR AIRCRAFT FLIGHT CONTROL RECONFIGURATION [J].

NAPOLITANO, MR ;

SWAIM, RL .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1991, 14 (01) :184-190

[10]

NOURA H, 1994, PROCEEDINGS OF THE THIRD IEEE CONFERENCE ON CONTROL APPLICATIONS, VOLS 1-3, P1397, DOI 10.1109/CCA.1994.381320

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