A near optimal midcourse guidance strategy with fixed-interval propulsive maneuvers for exoatmospheric interceptor is proposed. 本文针对大气层外中段拦截问题,设计了一种带有固定推进时间的近最优中制导策略。
A velocity-to-be-gained guidance law for exoatmospheric targets is proposed for an interceptor with a fuel-exhaustion-shutoff solid rocket motor. 针对拦截器使用耗尽关机固体燃料发动机的情况,设计了大气层外目标拦截的速度增益导引方法。
Terminal Guidance Study of Exoatmospheric(EXO) Spin Stabilized Interceptor 大气层外自旋稳定拦截器末制导控制研究
Effect of Earth Infrared Radiation on Infrared Temperature Measurement for Exoatmospheric(EXO) Objects 润红色,洋红(图画颜料)地球红外辐射对大气层外红外测温的影响
Guidance Based on Zero Effort Miss for Super-range Exoatmospheric(EXO) Intercept 基于零控脱靶量的大气层外超远程拦截制导