Quaternion-Based Reusable Launch Vehicle Composite Attitude Control Via Active Disturbance Rejection Control and Sliding Mode Approach (AIAA 2017-2320)
AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)
2017-01-01
14 pages
Conference paper
English
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Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle
Online Contents | 2006
|AIAA-2002-4779 Reusable Launch Vehicle Attitude Control Using Time-Varying Sliding Modes
British Library Conference Proceedings | 2002
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