摘要
以装备纵向数字电传操纵的某骏证机(简写成DFBW飞机,和相应的机械操纵飞机(简写成MCS飞机)为实例,采用时域对比方法,分析研究了该DFBW飞机在着陆过程中的纵向操纵特点,该飞机构形变化时的操纵特点及其对着陆特性的影响,从而得出一些符合实际情况的结论。
As an example, some verifying aircraft equipped with longitudinal digital flying—by—wire (DFBW) and its relevant aircraft with mechanical control system (MCS) are studied. Using a contrastive method of time domain, the longitudinal control characteristics of the DFBW aircraft during landing process, control characteristics in the aircraft configuration variation, and influence on its landing qualites are analyzed. Finally some practical conclusions weredrawn up and were conformed to reality. These conclusion are beneficial to new aircraft development and the pilots who are going to fly the aircraft equipped with DFBW.
出处
《飞行力学》
CSCD
北大核心
1993年第4期31-41,共11页
Flight Dynamics
关键词
数字电传操纵
飞机
着陆特性
Digital flying—by—wire aircrat Mechanical control system aircraft Control characteristic Aircraft configuration Landing quality
