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横向连续推力小偏心率人工冻结轨道设计
  • ISSN号：0254-6124
  • 期刊名称：空间科学学报
  • 时间：2012
  • 页码：555-559
  • 分类：V412.4[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术]
  • 作者机构：[1]宇航动力学国家重点实验室,西安710043, [2]西安卫星测控中心,西安710043, [3]清华大学航天航空学院,北京100084
  • 相关基金：国家自然科学基金资助项目（11072122）
  • 相关项目：火星轨道器动力学与稳定性研究
作者： 马庆甜|李俊峰|宝音贺西|
关键词： 卫星星座, WALKER星座, 星座控制, 轨道控制, satellite constellation, Walker constellation, constellation control, orbital control
中文摘要：

针对运行在中高轨道上的全球Walker星座的构形长期保持控制问题,通过分析星座卫星的轨道摄动及构形相对漂移,研究了星座构形长期保持的控制方法及控制策略.对于星座构形的保持,研究了星座构形摄动补偿法,提出了星座构形数值微分修正法.最后给出了全球星座构形长期保持控制策略并进行了仿真验证,仿真分析表明,星座构形数值微分修正法比构形摄动补偿法具有更高的控制计算精度.

英文摘要：

Aiming at orbital maintenance of the Walker constellation configuration in medium earth orbit considering the effects of orbital perturbation,we discuss the excursion of the constellation configuration.After this,the long-time maintenance control methods and the control strategy of the constellation configuration are discussed.The perturbation penalty method has been analyzed.The numerical differential modified method of the constellation configuration is presented and discussed.Finally,the long-time orbital control strategy for global constellation is presented and simulated.Simulation analysis shows that the constellation configuration numerical differential modified method can achieve higher control calculation accuracy than constellation configuration perturbation penalty method.

同期刊论文项目
火星轨道器动力学与稳定性研究
期刊论文 34
深空探测中若干非线性动力学与控制问题
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期刊信息
  • 《空间科学学报》
  • 北大核心期刊（2011版）
  • 主管单位:中国科学院
  • 主办单位:中科院空间中心
  • 主编：吴季
  • 地址：北京8701信箱
  • 邮编：100190
  • 邮箱：cjss@nssc.ac.cn
  • 电话：010-62582788
  • 国际标准刊号：ISSN：0254-6124
  • 国内统一刊号：ISSN：11-1783/V
  • 邮发代号:2-562
  • 获奖情况:
  • 核心期刊,中国期刊方阵“双效”期刊
  • 国内外数据库收录:
  • 俄罗斯文摘杂志,美国化学文摘（网络版）,英国科学文摘数据库,日本日本科学技术振兴机构数据库,中国中国科技核心期刊,中国北大核心期刊（2004版）,中国北大核心期刊（2008版）,中国北大核心期刊（2011版）,中国北大核心期刊（2014版）,中国北大核心期刊（2000版）
  • 被引量:3704