A novel rapid method to design optimal-fuel interplanetary trajectory for low-thrust propulsion is presented based on normal trajectory approach.
针对星际探测任务中燃料最省小推力转移轨道问题,提出一种基于标称轨道的快速设计方法。
C. electric propulsion system, Because of the rapid progress of power electrics and computer technique, electric propulsion systems on vessels have developed to a higher level.
由于电力电子技术和计算机技术的进展,使现代电力推进系统发生了很大变化。
应用推荐