摘要
参考Ｆ—１６战斗机数学模型和原始数据，通过分支分析和突变理论方法（ＢＡＣＴＭ）以及数值积分时间历程法的应用，估算出Ｆ—１６飞机的分支图。分析并参考飞机分支图特性，研究飞机深失速进入特性及其改出特性。考虑按随控布局概念设计的控制系统的应用，研究迎角反馈增益、俯仰均速度反馈增益和迎角／过载限制器中的增益等参数变化对Ｆ—１６飞机深失速特性的影响情况．
F-16 fighter mathematical model and its primary datas are referenced in this paper, the study ways involved the application of bifurcation analysis and calastropha theroy method (BACTM) and the usage of numerical integral time histories method to evaluate F-16 bifurcation diagram. Analyzing and referring bifurcation diagram's specific property, we study airplane deep-stall entry and recovery characteristics, considering the application of control system designed according to the idea of control configured vehicle (CCV), discussions are also made on the effects of control system parameters changes to F-16 deep-stall characteristics.
出处
《飞行力学》
CSCD
北大核心
1996年第4期19-24,共6页
Flight Dynamics
关键词
深失速
放宽静稳定性
飞行控制
仿真
战斗机
Deep-stall ,Relaxed statics stability, Bifurcation and calastropha theory ,Simulation
