Paper
1 February 1987 Stability Studies Of Solar Optical Telescope Dynamics
Sarma N. Gullapalli, Parimal K. Pal, Gregory P. Ruthven
Author Affiliations +
Proceedings Volume 0641, Acquisition, Tracking, and Pointing; (1987) https://doi.org/10.1117/12.964429
Event: 1986 Technical Symposium Southeast, 1986, Orlando, United States
Abstract
The Solar Optical Telescope (SOT) is designed to operate as an attached payload mounted on the Instrument Pointing System (IPS) in the cargo bay of the Shuttle Orbiter. Pointing and control of SOT is accomplished by an active Articulated Primary Mirror (APM), an active Tertiary Mirror (TM), an elaborate set of optical sensors, electromechanical actuators and programmable controllers. The structural interactions of this complex control system are significant factors in the stability of the SOT. The preliminary stability study results of the SOT dynamical system are presented. Structural transfer functions obtained from the NASTRAN model of the structure were used. These studies apply to a single degree of freedom (elevation). Fully integrated model studies will be conducted in the future.
© (1987) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Sarma N. Gullapalli, Parimal K. Pal, and Gregory P. Ruthven "Stability Studies Of Solar Optical Telescope Dynamics", Proc. SPIE 0641, Acquisition, Tracking, and Pointing, (1 February 1987); https://doi.org/10.1117/12.964429
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KEYWORDS
Actuators

Mirrors

Control systems

Gyroscopes

Sensors

Dynamical systems

Optical telescopes

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