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Proceedings Paper

CCD star tracker for attitude determination and control of a satellite for a space VLBI mission
Author(s): Kazuhide Noguchi; Koshi Sato; Ryouichi Kasikawa; Naoto Ogura; Keiken Ninomiya; Tatsuaki Hasimoto; Eiji Hirokawa
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Paper Abstract

This paper presents design and performance of a high- precision star tracker which has been developed for use in the attitude determination and control system of MUSES-B spacecraft; the space segment of space VLBI program called VSOP (equals VLBI Space Observation Program). The MUSES-B is being prepared for launch in September 1996. The attitude control system is required to fulfill an overall pointing accuracy of 0.01 degrees (3 sigma) of an 8 meter-diameter VLBI antenna mounted on the spacecraft. The onboard attitude determination system is based on a reset type Kalman filter that assures the overall attitude determination accuracy of 19 arcseconds, using outputs from the star trackers and the gyroscope-based inertial sensors. For this purpose, the star tracker is designed to provide star position detection accuracy of 4 arcsec random (1 sigma) plus 15 arcsec bias error. This paper describes the design of the STTs, the performance analyses, and ground test results of the Protoflight Model.

Paper Details

Date Published: 28 October 1996
PDF: 11 pages
Proc. SPIE 2810, Space Sciencecraft Control and Tracking in the New Millennium, (28 October 1996); doi: 10.1117/12.255141
Show Author Affiliations
Kazuhide Noguchi, NEC Corp. (Japan)
Koshi Sato, NEC Corp. (Japan)
Ryouichi Kasikawa, NEC Corp. (Japan)
Naoto Ogura, NEC Corp. (Japan)
Keiken Ninomiya, Institute of Space and Astronautical Science (Japan)
Tatsuaki Hasimoto, Institute of Space and Astronautical Science (Japan)
Eiji Hirokawa, Institute of Space and Astronautical Science (Japan)


Published in SPIE Proceedings Vol. 2810:
Space Sciencecraft Control and Tracking in the New Millennium
E. Kane Casani; Mark A. Vander Does, Editor(s)

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