摘要
提供了评估战斗机功能敏捷性的三种尺度──炸战周期时间，动态速率转弯图和相对能量状态，并以某机作为模型算例，用１８０°航向改机动动作，仿真计算了飞行员的操纵指令输入对功能敏捷性评估尺度的影响．算例模型包含了非线性全量运动方程，飞行控制系统和发动机的动力特性．因此，较为真实地反映了飞机的特性．
Three metrics evaluating fighter functional agility are presented. The metrics are Combat Cycle Time. Dynamic Speed Turn plots and Relative Energy State. The sensitivity of these metrics to the pilot control command is explored using nonlinear. non-real-time-six-degree of freedom generic computer simulation for a fighter aircraft. The program is high fidelity, containing full control system, engine power and aerodynamic models. The maneuver test are 180 degree heading angle change.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1995年第3期22-28,共7页
Journal of Beijing University of Aeronautics and Astronautics
关键词
歼击机
灵敏度
评价
操纵性
模拟仿真
fighter aircraft
sensitivity
evaluations
controllability (flight)
analog simulation
