Reusable Launch Vehicle Control in Multiple-Time-Scale Sliding Modes
Author:
Affiliation:
1. University of Alabama in Huntsville, Huntsville, Alabama 35899
2. NASA Marshall Space Flight Center, Huntsville, Alabama 35812
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/10.2514/2.4669
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5. Stability analysis of a continuous implementation of variable structure control
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