Lunar spacecraft powered descent control using higher-order sliding mode techniques

DOI10.1016/J.JFRANKLIN.2011.06.015zbMath1254.93053OpenAlexW1972091143MaRDI QIDQ1933437

Yuri B. Shtessel, Jeb S. Orr

Publication date: 24 January 2013

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2011.06.015

zbMATH Keywords

parametric uncertaintyrobust performanceexternal disturbancesflight control systemhigh order sliding mode (HOSM) control

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Variable structure systems (93B12)

Related Items (2)

Finite-time super-twisting sliding mode control for Mars entry trajectory tracking ⋮ Lunar spacecraft powered descent control using higher-order sliding mode techniques

Cites Work

• Unnamed Item
• Lunar spacecraft powered descent control using higher-order sliding mode techniques
• New methodologies for adaptive sliding mode control
• Sliding order and sliding accuracy in sliding mode control
• Higher-order sliding modes, differentiation and output-feedback control
• Universal single-input-single-output (SISO) sliding-mode controllers with finite-time convergence

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