NONLINEAR H-INFINITY CONTROL AND ITS APPLICATION TO RIGID SPACECRAFT

被引：113

作者：

KANG, W

机构：

[1] Mathematics Department, Naval Postgraduate School, Monterey CA

来源：

IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 1995年 / 40卷 / 07期

关键词：

D O I：

10.1109/9.400476

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The problem of H-infinity control of a rigid spacecraft with three control torques and disturbances is addressed. The Hamilton-Jacobi-Isaacs inequality for H-infinity feedback design is solved. An H-infinity suboptimal feedback is given, and the stability properties of the closed-loop system are studied.

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页码：1281 / 1285

页数：5

相关论文

共 15 条

[1]

BAILLIEUL J, 1975, THESIS HARVARD U CAM

[2] ON THE ATTITUDE STABILIZATION OF RIGID SPACECRAFT [J].

BYRNES, CI ;

ISIDORI, A .

AUTOMATICA, 1991, 27 (01) :87-95

[3] SPACECRAFT ATTITUDE-CONTROL AND STABILIZATION - APPLICATIONS OF GEOMETRIC CONTROL-THEORY TO RIGID BODY MODELS [J].

CROUCH, PE .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1984, 29 (04) :321-331

[4] PASSIVITY-BASED ADAPTIVE ATTITUDE-CONTROL OF A RIGID SPACECRAFT [J].

EGELAND, O ;

GODHAVN, JM .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1994, 39 (04) :842-846

[5]

Elgersma M. R., 1992, IEEE Control Systems Magazine, V12, P14, DOI 10.1109/37.158891

[6] THE ATTITUDE-CONTROL PROBLEM - COMMENTS [J].

FJELLSTAD, OE ;

FOSSEN, TI .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1994, 39 (03) :699-700

[7] PREDICTIVE MOMENTUM MANAGEMENT FOR THE SPACE STATION [J].

HATTIS, PD .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1986, 9 (04) :454-461

[8] DISTURBANCE ATTENUATION AND H-INFINITY-CONTROL VIA MEASUREMENT FEEDBACK IN NONLINEAR-SYSTEMS [J].

ISIDORI, A ;

ASTOLFI, A .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1992, 37 (09) :1283-1293

[9]

KANG W, 1994, P IEEE C DECIS CONTR

[10] HAMILTONIAN ADAPTIVE-CONTROL OF SPACECRAFT [J].

SLOTINE, JJE ;

DIBENEDETTO, MD .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1990, 35 (07) :848-852