| 注册
首页|期刊导航|国防科技大学学报|地心轨道引力波探测无拖曳系统平动控制策略

地心轨道引力波探测无拖曳系统平动控制策略

郝立维 张锦绣 王继河 张谕 孙玥

国防科技大学学报2024,Vol.46Issue(2):36-48,13.
国防科技大学学报2024,Vol.46Issue(2):36-48,13.DOI:10.11887/j.cn.202402004

地心轨道引力波探测无拖曳系统平动控制策略

Translational tracking strategy of drag-free system for gravitational wave detection in geocentric orbit

郝立维 1张锦绣 2王继河 2张谕 3孙玥4

作者信息

  • 1. 哈尔滨工业大学卫星技术研究所,黑龙江哈尔滨 150001
  • 2. 中山大学 航空航天学院,广东深圳 518107
  • 3. 中山大学天琴中心,广东珠海 519082
  • 4. 上海市空间智能控制技术重点实验室,上海 201109||上海航天控制技术研究所,上海 201109
  • 折叠

摘要

Abstract

An on-orbit drag-free control technique for spaceborne gravitational wave detection missions was discussed.Based on the analysis and design of a possible future geocentric orbit detection mission,the relative motion dynamics and coupling characteristics between the spacecraft and mass blocks of an on-orbit drag-free system with with two test masses were modeled.At the same time,the performance index and perturbation of the drag-free system in the mission were preliminarily analyzed,and a relative translational control law based on frequency domain H∞ optimal control theory was designed.Numerical simulation results show that when the test masses of the two-test-mass on-orbit drag-free system are arranged according to the breathing angle of laser rangefinder,without a fixed tracking point strategy and without suspension control input along the non-sensitive axis,the spacecraft can achieve tracking of the reference point while meeting the frequency domain performance index of the system.At the same time,the time domain displacement of each test mass can be controlled to the micron level,thus obtaining the pure gravitational reference required by the mission.

关键词

空间引力波探测/无拖曳控制/双检验质量/H∞控制

Key words

spaceborne gravitational wave detection/drag-free control/two-test-mass/H∞ theory

分类

航空航天

引用本文复制引用

郝立维,张锦绣,王继河,张谕,孙玥..地心轨道引力波探测无拖曳系统平动控制策略[J].国防科技大学学报,2024,46(2):36-48,13.

基金项目

广东省基础与应用基础研究重大资助项目(2019B030302001) (2019B030302001)

国防科技大学学报

OA北大核心CSTPCD

1001-2486

访问量0
|
下载量0
段落导航相关论文