Quaternion-Based Reusable Launch Vehicle Composite Attitude Control via Active Disturbance Rejection Control and Sliding Mode Approach
21st AIAA International Space Planes and Hypersonics Technologies Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2017
|Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle
Online Contents | 2006
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