Research on Control Augmentation System for a Flying Wing Aircraft
2014 ◽
Vol 1049-1050
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pp. 953-956
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Keyword(s):
Requirements of the longitudinal control augmentation system are presented through studying the 25thChina Civil Aviation Regulations and C* flight quality evaluation criterion; The C* control augmentation scheme commonly used in modern large airliners is adopted to design the control augmentation system due to the stability and handling problems for the flying wing aircraft; The particle swarm optimization algorithm is proposed due to the parameter-scheduling difficulties in the designed control augmentation system. Numerical simulation shows that the designed C* control augmentation scheme is feasible.
Proceedings of the ISCIE International Symposium on Stochastic Systems Theory and its Applications
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2010 ◽
Vol 2010
(0)
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pp. 304-309
2011 ◽
Vol 4
(8)
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pp. 261-263
2019 ◽
Vol 7
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pp. 904-906
2012 ◽
Vol 23
(7)
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pp. 1805-1815
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2010 ◽
Vol 29
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pp. 3273-3276