Attitude control system for the Extreme Ultraviolet Explorer Satellite.

Computer Science – Performance

Scientific paper

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Artificial Satellites:Control Systems

Scientific paper

The requirements, design, and expected performance of the Attitude Control Subsystem for the spin-stabilized Extreme Ultraviolet Explorer Satellite are presented. Computer simulations on the satellite dynamic response, pointing error, and stability during spin axis precession are given. Parameters that affect the pointing performance are also evaluated.

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