Reusable Launch Vehicle Control Using Linear-Adaptive and Subspace-Stabilization Techniques
Author:
Affiliation:
1. Davidson Enterprises, LLC, Huntsville, Alabama 35806
2. University of Alabama in Huntsville, Huntsville, Alabama 35899
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4710
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1. Guidance and control system using constrained adaptive backstepping method for space transportation;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-04-06
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3. Input-to-state-stability modular command filtered back-stepping attitude control of a generic reentry vehicle;International Journal of Control, Automation and Systems;2013-08
4. Hybrid adaptive ascent flight control for a flexible launch vehicle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-06-20
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