Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle
Author:
Affiliation:
1. NASA Marshall Space Flight Center
2. University of Alabama in Huntsville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6145
Reference28 articles.
1. 1NationalAeronauticsandSpaceAdministrationStrategicPlan,2004.
2. 3JamesW.McCarter,"MavericUser'sGuide",NASA,MSFCinternalmemorandum,1999.
3. New Nonlinear Control Technique for Ascent Phase of Reusable Launch Vehicles
4. Integrated Adaptive Guidance and Control for Re-Entry Vehicles with Flight Test Results
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