摘要
以将飞机准确、快速地引导到能够发现目标、进入战斗航向为目的,研究了机动指令生成的原理。以爬升俯冲为例,建立了导引机动指令的算法和控制模型。对程序接口进行了设计,同时对某型飞机快速爬升、程序爬升、俯冲下降和油门杆位置指令控制进行了仿真。其仿真结果验证了机动指令模型的合理性。
aimed to leading the aircraft to an airspace where it can find the target quickly and precisely,and aim at the battle course,then attack the target.The article have studied the principle of maneuver instruction generation,estab- lished the algorithm of guidance maneuver instruction and control model,designed program interface,and the process of fast climb and descent and the control of indicated-throttle lever are simulated,correct simulation have verified the rea- sonability of maneuver instruction model the research of guidance instruction model can be extensively applied in flight emulation.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第S4期443-445,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
机动指令
爬升俯冲
飞行仿真
作战效能
maneuver instruction
climb and descent
flight simulation
fight effectiveness
