NASA NTRS · 19830056215
A microprocessor-based position control system for a telescope secondary mirror
Abstract
The pointing requirements for the Shuttle IR Telescope Facility (SIRTF), which consists of an 0.85-m cryogenically cooled IR telescope, call for an image stability of 0.25 arcsec. Attention is presently given to a microprocessor-based position control system developed for the control of the SIRTF secondary mirror, employing a special control law (to minimize energy dissipation), a precision capacitive position sensor, and a specially designed power amplifier/actuator combination. The microprocessor generates the command angular position and rate waveforms in order to maintain a 90 percent dwell time/10 percent transition time ratio independently of chop frequency or amplitude. Performance and test results of a prototype system designed for use with a demonstration model of the SIRTF focal plane fine guidance sensor are presented.
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Lorell, K. R., Barrows, W. F., Clappier, R. R., Lee, G. K.. 1983-01-01. A microprocessor-based position control system for a telescope secondary mirror. https://ntrs.nasa.gov/citations/19830056215
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