Requirements of the longitudinal control augmentation system are presented through studying the 25th China 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.
Research on Control Augmentation System for a Flying Wing Aircraft
Advanced Materials Research ; 1049-1050 ; 953-956
2014-10-10
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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