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基于区域平均燃料消耗的推力器配置问题

王敏 王思野

空间控制技术与应用2018,Vol.44Issue(1):51-55,61,6.
空间控制技术与应用2018,Vol.44Issue(1):51-55,61,6.DOI:10.3969/j.issn.1674-1579.2018.01.007

基于区域平均燃料消耗的推力器配置问题

Thruster Configuration Problem Based on Regional Average Fuel Consumption

王敏 1王思野2

作者信息

  • 1. 北京控制工程研究所,北京100190
  • 2. 空间智能控制技术重点实验室,北京100190
  • 折叠

摘要

Abstract

To realize the high accuracy rendezvous and docking,the 6-degree orbit and attitude control is needed.For the same control command sequence,different thruster configurations and different control allocation algorithms lead to different fuel consumptions.As the control command sequence can be divided by time and space region,the regional average fuel consumption is proposed.The computing method of the regional average fuel consumption is given for both the 3-degree and the 6-degree control tasks.The optimal design method of the thruster configuration is suggested,which has important significance for thruster configuration design and control allocation.

关键词

推力器配置/燃料消耗/控制指令分配

Key words

thruster configuration/fuel consumption/control allocation

分类

航空航天

引用本文复制引用

王敏,王思野..基于区域平均燃料消耗的推力器配置问题[J].空间控制技术与应用,2018,44(1):51-55,61,6.

基金项目

国家自然科学基金资助项目(61403029)和国家重点基础研究发展计划(973)资助项目(2013CB733100).Supported by National Natural Science Foundation of China (61403029)and National Key Basic Research Program of China (2013CB733100). (61403029)

空间控制技术与应用

OA北大核心CSCDCSTPCD

1674-1579

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