Automatic Control of Launch Vehicles' Flight Path Slope Angle by Means of the Backstepping Control Method
Author:
Affiliation:
1. University of Craiova,Craiova,Romania
2. University of Craiova and University “Politehnica” of Bucharest,Romania
3. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10284032/10284045/10284261.pdf?arnumber=10284261
Reference31 articles.
1. Adaptive-gain fast super-twisting sliding mode fault tolerant control for a reusable launch vehicle in reentry phase
2. Optimal trajectory-tracking guidance for reusable launch vehicle based on adaptive dynamic programming
3. A fuzzy wavelet neural network-based approach to hypersonic flight vehicle direct nonaffine hybrid control
4. Design of a Robust Controller for Launch Vehicle
5. Auto-landing of UAVs with variable centre of mass using the backstepping and dynamic inversion control
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