摘要
研究了将飞机攻角影响引入进气道斜板调节系统的调节规律，仿真结果表明该调节规律使斜板调节系统具有良好的性能，对深入研究综合飞行／推进控制系统具有重要作用。
A new regulating method is proposed which includes the influence of angle of attack, and is used to design an inlet ramp regulating system. Simulations show that the method is satisfactory, and it is important for the research of integrated flight/propulsion control systems.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1997年第5期619-620,共2页
Acta Aeronautica et Astronautica Sinica
