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Robust model-based controller synthesis for the scole configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stewart, E. J. Armstrong, E. S. Joshi, S. M. |
| Copyright Year | 1988 |
| Description | 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. |
| File Size | 400629 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890004103 |
| Archival Resource Key | ark:/13960/t9188689s |
| Language | English |
| Publisher Date | 1988-10-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Dynamic Response Robustness Mathematics Control Systems Design Models Spacecraft Configurations Compensators Large Space Structures Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |