Optimization of fuzzy controller for minimum time response

Minimum time control is desired for non-linear spacecraft-satellite attitude systems to save on-board thruster fuel. The regulatory time depends on the initial attitude of the satellite. Bang-bang control of satellite attitude can be accomplished with fuzzy logic controller using largest of Maxima d...

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Bibliographic Details
Main Authors: Nagi F., Perumal L.
Other Authors: 56272534200
Format: Article
Published: Elsevier Ltd 2023
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