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GPS/VISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying 被引量：5

GPS/VISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying
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摘要 For the improvement of accuracy and better fault-tolerant performance, a global position system （GPS）/vision navigation （VISNAV） integrated relative navigation and attitude determination approach is presented for ultra-close spacecraft formation flying. Onboard GPS and VISNAV system are adopted and a federal Kalman filter architecture is used for the total navigation system design. Simulation results indicate that the integrated system can provide a total improvement of relative navigation and attitude estimation performance in accuracy and fault-tolerance. For the improvement of accuracy and better fault-tolerant performance, a global position system （GPS）/vision navigation （VISNAV） integrated relative navigation and attitude determination approach is presented for ultra-close spacecraft formation flying. Onboard GPS and VISNAV system are adopted and a federal Kalman filter architecture is used for the total navigation system design. Simulation results indicate that the integrated system can provide a total improvement of relative navigation and attitude estimation performance in accuracy and fault-tolerance.
作者 Xiaoliang Wang Xiaowei Shao Deren Gong Dengping Duan
机构地区 Institute of Aerospace Science & Technology
出处 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2011年第2期283-291,共9页 系统工程与电子技术（英文版）
关键词 control and navigation relative navigation federalKalman filter spacecraft formation flying global position system（GPS） vision navigation （VISNAV）. control and navigation, relative navigation, federalKalman filter, spacecraft formation flying, global position system（GPS）, vision navigation （VISNAV）.
分类号 V448.21 [航空宇航科学与技术—飞行器设计] V529.1 [航空宇航科学与技术—人机与环境工程]
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参考文献26

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同被引文献30

  • 1吴美平,逯亮清.北斗双星系统车辆定向技术[J].国防科技大学学报,2006,28(3):89-93. 被引量：6
  • 2解永春,张昊,石磊,孙承启.交会对接光学成像敏感器设计中的关键问题[J].航天控制,2006,24(5):35-39. 被引量：12
  • 3刘涛,解永春.基于GPS相对伪距差分的相对导航方法研究[J].中国空间科学技术,2007,27(1):1-8. 被引量：12
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引证文献5

二级引证文献11

Journal of Systems Engineering and Electronics
2011年 第2期

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