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
2017-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2017
|Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle
Online Contents | 2006
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