Presentation 2008-06-26
GPS pseudo range error analysis with precise ISS structure modeling between HTV and ISS navigation
Hiroyuki OHMINE, Takeshi YABUSHITA, Kazunari KIHIRA, Kota TANABE, Toru KASAI,
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Abstract(in English) Japan Aerospace Exploration Agency (JAXA) has been developing the H-II Transfer Vehicle (HTV). HTV is automated, unmanned logistic transporter to the International Space Station (ISS) and approaches to the ISS with relative navigation system from JEM-SIGI on JEM (Japanese Experiment Module) and HTV-SIGI on HTV to GPS (Global Positioning System). ISS structure has the possibility of serious impact on actual pseudo range and relative navigation by multipath influence. This paper describes the multipath analysis and pseudo range error analysis with ISS structure using the UTD technique. The delay paths are obtained by ray tracing method and pseudo range error analysis is estimated with Delay Lock Loop (DLL), and Good correlations between analysis and measurement of the pseudo range error with GPS simulator has been obtained and confirmed the validation of analysis. ISS Paddles and Radiators rotations are also included in the analysis model. Variation of communication level due to ISS structure is also analyzed in accordance with ISS and GPS trajectory.
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Keyword(in English) ISS / JEM / HTV / GPS / Pseudo range error / Multipath / DLL
Paper # SANE2008-24
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Conference Information
Committee SANE
Conference Date 2008/6/19(1days)
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Paper Information
Registration To Space, Aeronautical and Navigational Electronics (SANE)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) GPS pseudo range error analysis with precise ISS structure modeling between HTV and ISS navigation
Sub Title (in English)
Keyword(1) ISS
Keyword(2) JEM
Keyword(3) HTV
Keyword(4) GPS
Keyword(5) Pseudo range error
Keyword(6) Multipath
Keyword(7) DLL
1st Author's Name Hiroyuki OHMINE
1st Author's Affiliation Mitsubishi Electric Corporation()
2nd Author's Name Takeshi YABUSHITA
2nd Author's Affiliation Mitsubishi Electric Corporation
3rd Author's Name Kazunari KIHIRA
3rd Author's Affiliation Mitsubishi Electric Corporation
4th Author's Name Kota TANABE
4th Author's Affiliation Japan Aerospace Exploration Agency
5th Author's Name Toru KASAI
5th Author's Affiliation Japan Aerospace Exploration Agency
Date 2008-06-26
Paper # SANE2008-24
Volume (vol) vol.108
Number (no) 100
Page pp.pp.-
#Pages 6
Date of Issue