What is it about?
Design and analysis of a nonsingular terminal sliding mode controller for a small satellite with CEACS under the influence of flywheels considering system nonlinearity, uncertainties and disturbance.
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Why is it important?
It considers a nonlinear control approach for attitude control of a small satellite featuring Combined Energy and Attitude Control System in presence of uncertainties and disturbances
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This page is a summary of: Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS), Aerospace Science and Technology, May 2018, Elsevier,
DOI: 10.1016/j.ast.2018.02.006.
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