Presentation	1993/6/25 Bias-error Minimization Theorem for Geostationary Satellite Ranging/Orbit Determination Seiichirou Kawase,
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Abstract(in Japanese)	(See Japanese page)
Abstract(in English)	For the orbit determination of a geostationary satellite by two ranging stations,a useful fact was found out and proved:If the line connecting the two stations is perpendicular to the equatorial plane as viewed from the satellite,and if the tracking period equals the orbital period times and integer,then a ranging bias error will cause no more than a minimized constant longitudianal error in the orbit determination,with the errors in a,e,i, ascending node and perigee being all zero.Orbital accuracy improvement based on this fact is discussed,particularly for the control of multiple satellites crowding at the same orbital position.
Keyword(in Japanese)	(See Japanese page)
Keyword(in English)	satellite ranging / bias error / orbit determination accuracy
Paper #	SANE93-14
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Conference Information
Committee	SANE
Conference Date	1993/6/25(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)	Bias-error Minimization Theorem for Geostationary Satellite Ranging/Orbit Determination
Sub Title (in English)
Keyword(1)	satellite ranging
Keyword(2)	bias error
Keyword(3)	orbit determination accuracy
1st Author's Name	Seiichirou Kawase
1st Author's Affiliation	Communications Research Laboratory()
Date	1993/6/25
Paper #	SANE93-14
Volume (vol)	vol.93
Number (no)	120
Page	pp.pp.-
#Pages	8
Date of Issue