火力与指挥控制Issue(5)：73-78,6.
基于空间发射的远程交会路径规划
Trajectory Planning of Long-distance Rendezvous Based on Space Launch Technology
闫循良 1张金生 1廖守亿 1王仕成 1陈士橹2
作者信息
- 1. 第二炮兵工程大学，西安 710025
- 2. 西北工业大学，西安 710072
- 折叠
摘要
Abstract
Launching technology that space platform releases the chaser,together with trajectory planning of combined maneuver,is studied in this paper. Based on analysis on launch mode,launch window and initial launch attitude requirement,drop launch is chosen,and launch scheme is proposed as well. Aiming at the representative combined maneuver which is a long-distance rendezvous based on space launch technology,mission analysis is carried out. Nonlinear mathematical model for optimal multiple -impulsive rendezvous is given,and trajectory planning model subject to constraints is established for combined maneuver. A serial hybrid algorithm combining GA with SQP is designed. Moreover,the necessity analysis and simulation is carried out for launch scheme and parameters. Simulation results indicate that the analysis and strategies can availably implement the space launch mission design and trajectory planning for combined maneuver. Some results are valuable for applications on space operations.关键词
空间发射/远程交会/组合机动/路径规划/投放发射Key words
space launch/long-distance rendezvous/combined maneuver/trajectory planning/drop launch分类
航空航天引用本文复制引用
闫循良,张金生,廖守亿,王仕成,陈士橹..基于空间发射的远程交会路径规划[J].火力与指挥控制,2014,(5):73-78,6.
