Considering constraints of energy, time and line-of-sightangle, a near-range autonomous rendezvous glidescope orbit design method is studied based on the differential equation method.
考虑能量、时间、视线等约束条件，基于微分方程法研究了近程自主交会滑移轨道设计方法。
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For the case of planar interception, the so called relative heading error angle between the relative velocity vector and the LoS (LineofSight) is chosen as the output to be controlled to zero.