Control technology as applied to Space Telescope

Details Control technology as applied to Space Telescope Control technology as applied to Space Telescope

Jan 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981spie..295..146d&link_type=abstract

In: Control and communication technology in laser systems; Proceedings of the Twenty-fifth Annual International Technical Sympos

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Attitude Stability, Hubble Space Telescope, Laser Gyroscopes, Pointing Control Systems, Control Simulation, Guidance Sensors, Reaction Wheels, Structural Design Criteria, Torque

Scientific paper

The pointing control system (PCS) of the Space Telescope is addressed. The sensors employed in the primary PCS mode are the rate gyro assembly and the fine guidance sensors, while four reaction wheel assemblies provide control torques. Stability considerations based on structural modes are discussed, noting the stability margin criteria used in the design. Acquisition methodology is considered with regard to the PCS component hardware simulators and vehicle dynamics simulation.

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