超机动飞机的非线性动态逆控制

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1998, Vol. 19 ›› Issue (1): 45-49.

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NONLINEAR DYNAMIC INVERSION CONTROL FOR SUPER MANEUVERING AIRCRAFT

Zhu En¹, Guo Suofeng¹, Chen Chuande¹, Cai Weili²

1. Department of Automatic Control, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016;2. The Institute of Logistics Command, Beijing, 100858

Received:1996-12-23 Revised:1997-08-30 Online:1998-02-25 Published:1998-02-25

Abstract

Abstract:

A description is presented to the use of nonlinear dynamic inversion for the design of a flight control system for a super maneuverable aircraft. Then a nonlinear inversion controller was designed for the fast variables. This stabilized the longitudinal short period and improved the lateral directional responses over a wide range of angles of attack by use of a combination of areodynamic surfaces and the thrust vectoring control. Another nonlinear inversion controller was designed for the slow variables. It allows pilot to control the slow dynamics.

Key words: post -stall maneuver, nonlinear control, dynamic inversion

CLC Number:

Zhu En;Guo Suofeng;Chen Chuande;Cai Weili. NONLINEAR DYNAMIC INVERSION CONTROL FOR SUPER MANEUVERING AIRCRAFT[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(1): 45-49.

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NONLINEAR DYNAMIC INVERSION CONTROL FOR SUPER MANEUVERING AIRCRAFT

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