A fast design method for transfer orbit of lunar probe is presented using overlap conic curve method aimed at lunar landing transfer orbit and lunar satellite transfer orbit.
利用重疊圓錐曲線方法,針對著陸型和月球衛星型兩種地月轉移軌道,給出了一種地月轉移軌道的快速設計方法。
A fast design method for the lunar satellite transfer trajectory is presented by combining patched conic technique and ephemeris.
提出了一種將圓錐曲線拼接法與歷表相結合 ,快速設計月球衛星地月轉移軌道的方法。
Lunar satellite is the most popular concept in the recent and future lunar exploration missions, such as Clementine (NASA, 1994), Lunar Prospector (NASA, 1998) and Smart-1 (ESA, 2002).
發射月球衛星是探測月球的一個重要途徑,而且為了找水,多采用極軌方式。
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