飞机急滚运动的解耦控制

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (7): 841-846.

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THE DECOUPLING CONTROL FOR AIRPLANE IN RAPID ROLL

Hu Weiduo, Zhang Minglia, Wen Chuanyuan

Third Department,Beijing University of Aeronautics and Astronautics,Beuing,100083

Received:1992-11-26 Revised:1993-06-20 Online:1994-07-25 Published:1994-07-25

Abstract

Abstract: The control problem for airplane in rapid roll is analyzed.A 5-DOF model is used to derive a decoupling control law of roll,pitch and sideslip angle according to the nonlinear decoupling theory.The stability of the closed loop system is discussed.A method to stabilize the whole svstem when some fixed dYnamics are unstable is given. At last,simulations are perfonned.

Key words: nonlinear systems, input/output routines-decoupling, stability, dynamic re-sponse

CLC Number:

Hu Weiduo;Zhang Minglia;Wen Chuanyuan. THE DECOUPLING CONTROL FOR AIRPLANE IN RAPID ROLL[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(7): 841-846.

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THE DECOUPLING CONTROL FOR AIRPLANE IN RAPID ROLL

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