CAJ | 학술논문

在满足对目标卫星在指定时间进行拦截的要求下，考虑拦截器变轨能量消耗最省，提出了基于定时拦截的在轨机动拦截轨道选择与优化方法。该方法能够迅速设计和优化出最优在轨机动拦截轨道、变轨点位置和变轨所需的能量。仿真结果表明，模型准确、有效，能够满足作战要求。
재만족대목표위성재지정시간진행란절적요구하，고필란절기변궤능량소모최성，제출료기우정시란절적재궤궤동란절궤도선택여우화방법。해방법능구신속설계화우화출최우재궤궤동란절궤도、변궤점위치화변궤소수적능량。방진결과표명，모형준학、유효，능구만족작전요구。
Given the minimum energy consumption of space based weapon transfer, A method which designs and optimizes the interception transfer path base on the schedule interception time is put forward. The interception transfer path, transfer position and energy consumption of transfer can be designed and optimized rapidly by this method. The model and algorithm is accurate and effective and satisfies the operational requirement indicated through the simulation result.