摘要
分析了敏捷性与飞控系统控制律之间的关系。以某典型三代机为例,根据飞行品质要求对其控制律进行了重新设计,并在地面仿真系统上对与控制律相关的敏捷性尺度进行了试验。通过比较原飞机和采用新控制律飞机的敏捷性,验证了分析结果,并对控制律提出了改进意见。
The relationships between agilities and flight control law （FCL） are analyzed. The FCL of a typical 3rd generation fighter is redesigned based on the requirements of flying qualities. The agility metrics relative to FCL are evaluated by pilot operation on a ground-based simulator. By comparing the agility evaluating results of the original aircraft and the aircraft with new FCL, the analysis is validated, and the adviees to improve the FCL are proposed.
出处
《飞行力学》
CSCD
北大核心
2008年第6期1-5,共5页
Flight Dynamics
