摘要
针对F-22A战机大机动、强突防、高隐身等能力特性对现代空战带来的新威胁,在选取合理的两种坐标系并建立战机质心运动方程的基础上,通过对3种典型机动模式下飞行航迹的数字仿真,较准确地掌握了F-22A战机在大机动情况的飞行能力,为空战过程中有效实施对F-22A战机的拦截行动提供了理论参考。
This paper focuses on the new threats to the modern air combat caused by the characteristics of the F-22A fighter’s large maneuvering,high penetration and high stealth capabilities.It selects two kinds of reasonable coordinate systems and establishes the fighter’s centroid equations of motion.The digital simulation of the flight trajectory under three typical maneuvering modes accurately captures the F-22A fighter’s ability of flying in large maneuvers.And the effective implementation of the F-22A fighter interception action provides a theoretical reference in an air combat process.
作者
赵思源
李小兵
何阳光
李兴格
ZHAO Si-yuan;LI Xiao-bing;HE Yang-guang;LI Xing-ge(Air and Missile Defense College,Air Force Engineering University,Xi'an 710051,China)
出处
《飞行力学》
CSCD
北大核心
2018年第6期21-24,共4页
Flight Dynamics
基金
国家自然科学基金资助(61603410)
关键词
飞行仿真
机动模式
空战
flight simulation
maneuvering mode
air combat
