Trajectory optimization design of a lunar polar probe

被引：0

作者：

Zhang, ZM ^{[1
]}

Sun, ZW ^{[1
]}

Yang, D ^{[1
]}

机构：

[1] Harbin Inst Technol, Dept Space Engn & Mech, Harbin 150006, Peoples R China

来源：

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY | 2003年 / 75卷 / 01期

关键词：

probes; design; research; flight; space;

D O I：

10.1108/00022660310457275

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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.

引用

页码：33 / 37

页数：5

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