Application of discrete time sliding mode control to a spacecraft in 6DoF with parameter identification

DOI10.1080/00207179.2010.510173zbMath1210.93046OpenAlexW2059412890MaRDI QIDQ5391438

Nicholas K. Lincoln, Sandor M. Veres

Publication date: 6 April 2011

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

Full work available at URL: https://doi.org/10.1080/00207179.2010.510173

zbMATH Keywords

discrete sliding mode controlspacecraft controlautonomous controlsix degrees of freedom

Mathematics Subject Classification ID

System identification (93B30) Discrete-time control/observation systems (93C55) Variable mass, rockets (70P05) Variable structure systems (93B12)

Related Items (3)

Guidance law and neural control for hypersonic missile to track targets ⋮ Inverse optimal sliding mode control of spacecraft with coupled translation and attitude dynamics ⋮ New design methodology for adaptive switching gain based discrete-time sliding mode control

Cites Work

• Spacecraft attitude control using explicit model predictive control
• Mass property estimation for control of asymmetrical satellites
• The attitude control problem
• Universal adaptive control of satellite formation flying
• Attitude control without angular velocity measurement: a passivity approach
• Components of a vision assisted constrained autonomous satellite formation flying control system

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