The miss distance caused by guidance method error and the effects of perturbation are compensated in this initial guidance law 該初制導方法能補償制導方法誤差和軌道攝動對攔截脫靶量的影響。
In this paper , the precise initial guidance law based on velocity gain guidance and the state transition matrix for orbit interception were proposed 摘要對于軌道攔截問題,給出了一種基于速度增益制導和狀態(tài)轉(zhuǎn)移矩陣的精確初制導方法。