摘要
讨论了利用飞行控制系统对静不稳定飞机的三种补偿方式：延迟俯仰速率反馈、迎角反馈和法向过载负反馈。从而改变了飞机特性，诸如减轻质量，提高升阻比，增强机动性等。最后对三种补偿方案进行了比较，采用迎角反馈补偿是最直接有效的手段，但在工程实践中，往往采用俯仰率和迎角混合反馈补偿方式。
As developing of the active control technology(ACT),the airframe can bedesigned as unstable configuration. This paper study and compare the three compensativeways of RSS airframe with the flight control system,delay pitch rate,angle of attack andnormal acceleration feedback. It is of pratical use in engineering.
出处
《飞行力学》
CSCD
北大核心
1995年第2期40-44,共5页
Flight Dynamics
