Presentation 1993/9/30
MUSES-B Navigation
Takaji Kato, Tsutomu Ichikawa,
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Abstract(in Japanese) (See Japanese page)
Abstract(in English) The Institute of Space and Astronautical Science plans to launch the S-VLBI(Space Very Long Baseline Interferometry)satellite named MUSES-B into an eccentric orbit with 20,000km apogee height and 1, 000km perigee height in 1996.The S-VLBI includes a satellite as one of the received stations in order to get high resolution maps of radio sources.The requirements of orbit determination is very stringent.This satellite can be observed S-band range and 2-way coherent doppler data at one station and Ku-band 2-way coherent doppler data at another station at the same time.In this paper we describe characteristic of accuracy for the navigation and numerical results.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) Orbit determination / MUSES-B / VLBI / Doppler / Kalman filter
Paper # SANE93-38
Date of Issue

Conference Information
Committee SANE
Conference Date 1993/9/30(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) MUSES-B Navigation
Sub Title (in English)
Keyword(1) Orbit determination
Keyword(2) MUSES-B
Keyword(3) VLBI
Keyword(4) Doppler
Keyword(5) Kalman filter
1st Author's Name Takaji Kato
1st Author's Affiliation The Institute of Space and Astronautical Science()
2nd Author's Name Tsutomu Ichikawa
2nd Author's Affiliation The Institute of Space and Astronautical Science
Date 1993/9/30
Paper # SANE93-38
Volume (vol) vol.93
Number (no) 254
Page pp.pp.-
#Pages 8
Date of Issue