摘要
介绍了迎角过载边界限制器的意义、设计要求和一些有代表性的国内外飞机的边界限制器设计方法。边界限制经历了硬限制、软限制、反馈限制和比较逻辑反馈限制几个阶段。分析了这些设计方法的优缺点,并对比较逻辑反馈限制器的设计方法进了理论推导,提出了这类边界限制器重要参数的确定方法。
A description is given to the importance and designing demand for the limiter of angle of attack and normal acceleration( AOA limiter ) as well as some design methods utilized in foreign aircraft and domestic aircraft . The advantages and disadvantages of these methods are analyzed, and some work is done in logic feedback limiter′s design method. A method is introduced to calculate the parameters in the limiter. It is a useful way to ensure normal design of boundary limiters.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1995年第1期87-91,共5页
Acta Aeronautica et Astronautica Sinica
关键词
迎角
控制
加速度
飞机
边界限制器
angle of attack, control, acceleration (physics)