Trajectory optimization design of a lunar polar probe
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 February 2003
Abstract
This article presents the optimized design, analysis and calculation concerning the trajectory of a lunar polar probe. Firstly, the trajectory design principles and constraints are determined. The preliminary design and analysis of the circumlunar orbit, transfer orbit to the moon and earth parking orbit are carried out separately and some computations for the flight trajectory concept have been made too. To reduce the fuel needed for error in orbital maneuver efficiently and satisfy the requirements on the launch window, some detailed design and analysis for the rather advanced phasing earth‐moon transfer orbit are given here and also the strategy for optimum orbit correction.
Keywords
Citation
Zhenmin, Z., Zhaowei, S. and Di, Y. (2003), "Trajectory optimization design of a lunar polar probe", Aircraft Engineering and Aerospace Technology, Vol. 75 No. 1, pp. 33-37. https://doi.org/10.1108/00022660310457275
Publisher
:MCB UP Ltd
Copyright © 2003, MCB UP Limited