Design UCAV Flight Control Law Based on Jamming Observer

Hai Wen Du; Xing Wei Weng; Yu Song Fu; Chuan Lin Tang

doi:10.4028/www.scientific.net/AMM.66-68.27

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 66-68Design UCAV Flight Control Law Based on Jamming...

Design UCAV Flight Control Law Based on Jamming Observer

Abstract:

In order to study the nonlinear jamming problem in UCAV’s flight control system, a method of using observer to check the system’s jamming was designed, constructed robust dynamic inversion control law based on jamming observer. The simulation results show that the robust dynamic inversion control law based on jamming observer, make UCAV’s flight control system have good stability and robustness, it’s a great convenience analyzing the system stability.

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Periodical:

Applied Mechanics and Materials (Volumes 66-68)

Pages:

27-30

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.66-68.27

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Online since:

July 2011

Authors:

Hai Wen Du, Xing Wei Weng, Yu Song Fu, Chuan Lin Tang

Keywords:

Control Law, Dynamic Inversion, Jamming Observer, Nonlinear System

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