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.
Robust Model-Based Controller Synthesis for the SCOLE (Space Control Laboratory Experiment) Configuration
1988
7 pages
Report
No indication
English
Robust model-based controller synthesis for the SCOLE configuration
Tema Archive | 1988
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