2017 25th Mediterranean Conference on Control and Automation (MED) 2017
DOI: 10.1109/med.2017.7984289
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Application of decaying boundary layer and switching function method thorough error feedback for sliding mode control on spacecraft's attitude

Abstract: Abstract-Effective operation of small spacecraft implies processors with low cost, energy efficiency and low computational burdens while retaining accurate output tracking. This paper presents the extension of work in [1] on eliminating the chattering for Sliding Mode Control (SMC) using a decaying boundary layer design which is able to achieve these small spacecraft operation needs. The extension is applied on a spacecraft's attitude control, while orbiting the earth with angular velocity, ω0. In SMC, chatter… Show more

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Cited by 7 publications
(2 citation statements)
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“…Another consideration for the SMC is to reduce the chattering of control inputs. Chattering refers to the switching of a variable from a control input around a reference point in a short period of time, which cannot be applied to an input from the actual system, and thus leads to the introduction of the concept of the boundary layer [41]. To apply the boundary layer concept, the existing signum function was replaced with the saturation function.…”
Section: Design Of a Sliding Mode Controlmentioning
confidence: 99%
“…Another consideration for the SMC is to reduce the chattering of control inputs. Chattering refers to the switching of a variable from a control input around a reference point in a short period of time, which cannot be applied to an input from the actual system, and thus leads to the introduction of the concept of the boundary layer [41]. To apply the boundary layer concept, the existing signum function was replaced with the saturation function.…”
Section: Design Of a Sliding Mode Controlmentioning
confidence: 99%
“…Another approach found in the literature for dealing with parametric uncertainties is the SMC [17][18][19][20][21][22]. It is a robust control approach as it is unresponsive to external disturbances and parametric uncertainties or variations [23,24].…”
mentioning
confidence: 99%