Sliding-mode control system for the three-axis attitude control of rigid-body spacecraft with unknown dynamics parameters

DOI10.1080/00207179108934184zbMath0749.93041OpenAlexW2151326153MaRDI QIDQ3980069

Alison B. Walker, Stephen J. Dodds

Publication date: 26 June 1992

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207179108934184

zbMATH Keywords

sliding-mode approach

Mathematics Subject Classification ID

Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

Robust attitude tracking control of spacecraft under unified actuator dynamics ⋮ Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques

Cites Work

• Continuous approximation of variable structure control
• Unnamed Item

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