An optimal orbit maneuver method based on continuous lowthrust was presented to solve relative motion control.
针对近距离相对运动的轨道控制问题，提出用常值小推力完成最优转移的方法。
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This paper makes an undated assessment of the technical and economic feasibility of transferring satellites from low Earth Orbit to Geostationary Orbit using lowthrust propulsion.
本文对利用低推力推进装置将卫星从低地轨道转移到静地轨道的可行性在技术上和经济上重新作了评价。
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Then the paper applies EA and SPEA to an orbital transformation problem. - time-energy optimization o The paper also solve lowthrust control problem of relative motion using fuzzy logic.