Nonlinear control law design for high angle of attack flight

Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

Volumn 24, Issue 1, 2006, Pages 35-39

  Zhang, Yizhe ^a   Deng, Jianhua ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Flight control; High angle of attack; Nonlinear control law design; Thrust vectoring

Indexed keywords

AIRCRAFT; COMPUTER SIMULATION; NONLINEAR CONTROL SYSTEMS; VECTORS;

FLIGHT CONTROL; SYSTEM DESIGN; THRUST VECTORING;

FLIGHT DYNAMICS;

EID: 33744730826     PISSN: 10002758     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. Beh H, Hofinger G, Huber P. Control Law Design and Flight Test Results of the Experimental Aircraft X-31A. In: Tischler Mark B. Advances in Aircraft Flight Control. Published by Taylor and Francis, London, 1996
2. Beh H, Bunt R Van D, Fisher B. High Angle of Attack Approach and Landing Control law Design for the X-31A. AIAA 2002-0247
3. Walker Gregory P, Allen David A. X-35B STOVL Flight Control Law design and Flying Qualities. AIAA 2002-6018
4. Reiner Jacob, Balas Gary J, Garrard William L. Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft. Journal of Guidance Control and Dynamics, 1995, 18(1)
5. Reiner Jacob, Balas Gary J, Garrard William L. Flight Control Design Using Robust Dynamic Inversion and Time-Scale Separation. Automatica, 1996, 32(11): 1439