摘要
针对现代作战飞机方案评估和设计的要求,构建了现代空战仿真系统中计算机控制的飞机仿真基本框架。根据现代空战中典型机动动作对速度矢量的指向要求,从控制飞机速度矢量出发,建立了一类空战机动动作控制的基础模型,并对能反映飞机性能的限制环节进行了建模。仿真结果表明,利用该模型对飞机进行方案评估和性能指标设计是合理的,所建模型能够较好地仿真空战机动,体现飞机性能指标对空战机动的影响。
For the evaluation of fighter＇ s conceptual design, the frame of autonomous air combat simulation is constructed. Based on fighter＇ s velocity control, the common model of maneuver autopilot is developed. This paper also presented the models of limit module that reveals the fighter＇ s performance. Simulation results show that the models are effective to maneuver simulation and performance evaluation for modern fighters.
出处
《飞行力学》
CSCD
北大核心
2007年第1期34-38,共5页
Flight Dynamics
关键词
空战仿真
机动控制
性能指标
方案评估
air combat simulation
maneuver autopilot
performance index
evaluation of conceptual design
