Analysis of the Divert Ability of Atmospheric Interceptors Controlled by Lateral Jet Thrusters
In order to analyze the divert ability of atmospheric interceptors controlled by lateral jet thrusters, the models of two kinds of atmospheric interceptors are established: one is with attitude control thrusters, the other is with divert thrusters. Considering overload response time, consumptions of thrusters and time-to-go, maximal terminal divert distances are formulated for tracking a step input under several flight conditions. Finally, based on the above results, considering two types of missiles with typical parameters, their corresponding battle skies, where their divert abilities can be utilized, are given.
Atmospheric Interceptor Lateral Jet Thrusters Divert Ability Pulse Jet Control Battle Sky
Yu Yao Yongtao Bi Yuhang Wang
Control and Simulation Center, Harbin Institute of Technology, Harbin 150080, China
国际会议
2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)
广西桂林
英文
2399-2403
2009-06-17（万方平台首次上网日期，不代表论文的发表时间）