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。
By investigating the waveguiding characteristics of gain-guided fibers, the cutoff conditions of different modes as function of gain-coefficient and index step are obtained.
分析了增益导引光纤中,增益因子对折射率以及归一化频率的影响,得到了光纤中各阶模式截止条件与芯包层折射率差和增益因子的关系。
