Abstract
CONTROLLER design is more troublesome in aerospace systems due to, inter alia, diversity of mission platforms, convoluted nonlinear dynamics, predominantly strict mission and resource constraints, and demands for guaranteed operability within a wide range of operating conditions that can undergo structural or unexpected changes. Most of the space systems (e.g., planetary observers, rovers, space telescopes, spacecraft optical systems, etc.) require studious design, production, and testing processes. Indeed, space systemsare required to endure a wide spectrumof environmental changes with limited resources and are typically subject to partial, highly expensive, or even nonexistent service or repair. Clearly, aerospace missions induce high cost, require long development times as well as long mission lifespan, and demand high-fidelity operation so that, not surprisingly, related control tasks are significantly more demanding in aerospace compared to many other industries.
Original language | English |
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Pages (from-to) | 1541-1566 |
Number of pages | 26 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 40 |
Issue number | 7 |
DOIs | |
Publication status | Published - 2017 |
Bibliographical note
Funding Information:This research was supported by the Ministry of Education, Singapore, with the project title "Model Predictive Control-Moving Horizon Estimation Framework as Applied to Tilt Rotor UAVs and Its Experimental Evaluation", grants RG191/14, by U.S. National Science Foundation grants CMMI-1613235 and CNS-1619729, Office of Naval Research grant N00014-16-1-2318, U.S. Air Force contract FA8650-15-C-2546, and the Foundation for Science and Technology of Portugal under grant PTDC/EEI-AUT/ 2933/2014.
Publisher Copyright:
Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc.