• DocumentCode
    691180
  • Title

    Relative Navigation and Guidance Technologies for Rendezvous and Docking

  • Author

    An Kai ; Tang Zhaoting

  • Author_Institution
    Shandong Aerosp. Electro-Technol. Inst., Yantai, China
  • fYear
    2013
  • fDate
    21-23 Sept. 2013
  • Firstpage
    1228
  • Lastpage
    1232
  • Abstract
    Relative navigation and guidance is a key operational technology required for rendezvous and docking. This paper intends to describe and review some recent patents related to the methods and devices of relative navigation and guidance, including laser guidance, GNSS and UWB guidance, and relative navigation using laser range finder. Corresponding to each of these patents, some reformative approaches and methods are presented in the paper. Especially, a method based on Hill equation is presented which can produce a state estimate to replace the interrupted the visible sensor measurement when, for example, the target satellite is in shadow and the Sun´s rays do not illuminate the target.
  • Keywords
    Global Positioning System; aircraft landing guidance; artificial satellites; laser ranging; photodetectors; state estimation; ultra wideband technology; GNSS; Hill equation; UWB guidance; docking; laser guidance; laser range finder; photodetector; reformative approach; relative navigation; rendezvous; state estimation; visible sensor measurement; Distance measurement; Global Positioning System; Measurement by laser beam; Semiconductor lasers; Space vehicles; Relative navigation; relative position; relative velocity; rendezvous and docking;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2013 Third International Conference on
  • Conference_Location
    Shenyang
  • Type

    conf

  • DOI
    10.1109/IMCCC.2013.273
  • Filename
    6840663