摘要
主要考虑大迎角非定常气动力对飞控系统的影响，并给出在动态逆飞行控制系统中抑制这种影响的方法。非定常气动力表现在气动参数上是出现滞环现象，本文根据已有的成果。
Discusses how the unsteady aerodynamics of airplane influence in flight control system at high angles of attack,and gives out a method for processing the influence in a dynamic inversion flight control system,unsteady aerodynamics has a slugglish loop phenomenon at areodynamics parameters. This paper mainly discusses some problems about longitudinal flight control with the results which had been studied.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
1998年第5期584-587,共4页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
非定常气动力
飞行控制系统
动态逆方法
unsteady aerodynamic
flight control systems
dynamic inversion method
