Modelling and fault tolerant control for near space vehicles with vertical tail loss

Author:

Zhao Jing1,Jiang Bin1,He Zhen1,Mao Zehui1

Affiliation:

1. College of Automation Engineering, Nanjing University of Aeronautics and AstronauticsNanjing210016People's Republic of China

Funder

National Natural Science Foundation of China

National Aerospace Science Foundation of China

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Reference38 articles.

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2. Intelligent adaptive control of a tailless advanced fighter aircraft under wing damage;Boškvić J.D.;J. Guid. Control Dyn.,2000

3. Nonlinear Reconfiguring Flight Control Based on Online Physical Model Identification

4. LombaertsT.J.HuismanH.O.ChuQ.P.MulderJ.A. andJoostenD.A.: ‘Computer based real‐time damaged aircraft model identification with two step method and modified stepwise regression’.The 18th Symp. of the Society of Flight Test Engineers—European Chapter TUD 2007.

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