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)
01.01.2017
14 pages
Aufsatz (Konferenz)
Englisch
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Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle
Online Contents | 2006
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British Library Conference Proceedings | 2002
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