Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle
Author:
Affiliation:
1. NASA Marshall Space Flight Center, Huntsville, Alabama 35812
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/10.2514/1.20151
Reference31 articles.
1. Advanced Guidance and Control Methods for Reusable Launch Vehicles: Test Results
2. New Nonlinear Control Technique for Ascent Phase of Reusable Launch Vehicles
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