2008•Journal of AstronauticsRequires access

Fast Searching Design Method for Return Transfer Trajectory of Lunar Probe

Lei Liu

Abstract

According to the multi-constraints of the return transfer trajectory for special engineering requirements,a fast searching method for the return trajectory of lunar probe is designed,in which a series analytical model is founded under the idealized double two-body hypotheses and dichotomy is used to search the orbit.The searching method is efficiency and the output can be the well initial value for the orbit precision design.The method has theoretical purpose and application value for the return required lunar probe engineering.

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Key concepts: Trajectory, Series (stratigraphy), Orbit (dynamics), Lunar orbit, Computer science, Aerospace engineering, Algorithm, Control theory (sociology)