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Autonomus navigation for spacecraft using GPS sensor
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- Mitsutake Masaaki
- Space systems division,Hitachi,ltd
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- Kosaka Michitaka
- Systems development laboratory,Hitachi,ltd
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- Kato Takaji
- Institute of space and astronavtical science
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- Ichikawa Tsutomu
- Institute of space and astronavtical science
Bibliographic Information
- Other Title
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- GPSを用いた人工衛星の自律航法
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Description
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.
Journal
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- Technical report of IEICE. SANE
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Technical report of IEICE. SANE 93 (540), 17-23, 1994-03-25
The Institute of Electronics, Information and Communication Engineers
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Keywords
Details 詳細情報について
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- CRID
- 1570854177430585984
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- NII Article ID
- 110003289419
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- NII Book ID
- AN10013301
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- Text Lang
- ja
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- Data Source
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- CiNii Articles
