NASA NTRS · 19890004103
Robust model-based controller synthesis for the SCOLE configuration
Abstract
The design of a robust compensator is considered for the SCOLE configuration using a frequency-response shaping technique based on the LQG/LTR algorithm. Results indicate that a tenth-order compensator can be used to meet stability-performance-robustness conditions for a 26th-order SCOLE model without destabilizing spillover effects. Since the SCOLE configuration is representative of many proposed spaceflight experiments, the results and design techniques employed potentially should be applicable to a wide range of large space structure control problems.
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Armstrong, E. S., Joshi, S. M., Stewart, E. J.. 1988-10-01. Robust model-based controller synthesis for the SCOLE configuration. https://ntrs.nasa.gov/citations/19890004103
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