To consider the effect of the earth on the calculation of ultra range trajectory more accurately, an elliptic earth trajectory model adopting accurate normal gravity is established.
为了更精确地考虑地球对超远程弹道计算的影响,提出了一个计入精确正常重力的椭球地表弹道模型。
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。
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