Nonlinear Stochastic Control Part II: Ascent Phase Control of Reusable Launch Vehicles
Author:
Affiliation:
1. University of Central Florida
2. Mississippi State University
3. University of Oklahoma
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-5956
Reference28 articles.
1. Dynamic Inversion-Based Adaptive/Reconfigurable Control of the X-33 on Ascent
2. Reusable Launch Vehicle Control in Multiple-Time-Scale Sliding Modes
3. New Nonlinear Control Technique for Ascent Phase of Reusable Launch Vehicles
4. Limited Authority Adaptive Flight Control for Reusable Launch Vehicles
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2. Reentry attitude control for a reusable launch vehicle with aeroservoelastic model using type-2 adaptive fuzzy sliding mode control;International Journal of Robust and Nonlinear Control;2018-09-25
3. Nonsingular finite-time second order sliding mode attitude control for reentry vehicle;International Journal of Control, Automation and Systems;2015-05-23
4. Finite-time sliding mode attitude control for a reentry vehicle with blended aerodynamic surfaces and a reaction control system;Chinese Journal of Aeronautics;2014-08
5. Smooth second-order nonsingular terminal sliding mode control for reusable launch vehicles;International Journal of Intelligent Computing and Cybernetics;2014-03-04
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