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Nonlinear inverse dynamics control of the aircraft in the presence of windshear

Yihua Cao (Beijing University of Aeronautics and Astronautics, Beijing, People's Republic of China)
Yong Chen (Beijing University of Aeronautics and Astronautics, Beijing, People's Republic of China)
Kungang Yuan (Beijing University of Aeronautics and Astronautics, Beijing, People's Republic of China)
Changjiang Jin (Beijing University of Aeronautics and Astronautics, Beijing, People's Republic of China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 December 2004

Abstract

Control laws that are based on the nonlinear inverse dynamics (NID) of the aircraft offer the potential for providing improved levels of performance over conventional flight control designs. The NID and its application in the flight control during windshear penetration are introduced here. With the employment of a real engineering windshear model and NID, a low‐altitude windshear penetration flight control law is designed. The simulative calculation results indicated that the NID control logic works effectively in the trajectory control of the aircraft during the penetration of windshear.

Keywords

Citation

Cao, Y., Chen, Y., Yuan, K. and Jin, C. (2004), "Nonlinear inverse dynamics control of the aircraft in the presence of windshear", Aircraft Engineering and Aerospace Technology, Vol. 76 No. 6, pp. 592-599. https://doi.org/10.1108/00022660410565517

Publisher

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Emerald Group Publishing Limited

Copyright © 2004, Emerald Group Publishing Limited