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VTVL Launch Vehicle Control Method by tranduc20031611 is a document available to read on EtoBox.
This paper presents a fixed-time extended state observer based non-singular fast terminal sliding mode control for a vertical take-off and vertical landing (VTVL) reusable launch vehicle. It develops a six-degree-of-freedom dynamic model and proposes a novel control scheme that estimates error states and disturbances, ensuring robust performance in the presence of uncertainties. The effectiveness of the proposed control strategy is demonstrated through numerical simulations.
- Author
- tranduc20031611
- Language
- EN