Presentation 1994/3/25
Autonomus navigation for spacecraft using GPS sensor
Masaaki Mitsutake, Michitaka Kosaka, Takaji Kato, Tsutomu Ichikawa,
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Abstract(in Japanese) (See Japanese page)
Abstract(in English) The reaftime attribute and autonomy as well as high precision are required for the navigation and guidance system of future spacecrafts.When a spacecraft travels along a near earth orbit, these requirements are considered to be fuffilled by using GPS(Global Positioning System)for the navigation and guidance system.Autkors have recently developed an autonomous navigation fitter which can output the orbital parameters of an earth orbiting satellite with a stable precision,and installed if in a satellite borne GPS navigation sensor.This paper reports the results of the performance testing of the autonomous navigation filter developed.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) GPS / Navigation filter / Avtonomous
Paper # SANE93-103
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Conference Information
Committee SANE
Conference Date 1994/3/25(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) Autonomus navigation for spacecraft using GPS sensor
Sub Title (in English)
Keyword(1) GPS
Keyword(2) Navigation filter
Keyword(3) Avtonomous
1st Author's Name Masaaki Mitsutake
1st Author's Affiliation Space systems division,Hitachi,ltd()
2nd Author's Name Michitaka Kosaka
2nd Author's Affiliation Systems development laboratory,Hitachi,ltd
3rd Author's Name Takaji Kato
3rd Author's Affiliation Institute of space and astronavtical science
4th Author's Name Tsutomu Ichikawa
4th Author's Affiliation Institute of space and astronavtical science
Date 1994/3/25
Paper # SANE93-103
Volume (vol) vol.93
Number (no) 540
Page pp.pp.-
#Pages 7
Date of Issue