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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主要な著者: | Nagi F., Perumal L. |
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その他の著者: | 56272534200 |
フォーマット: | 論文 |
出版事項: |
Elsevier Ltd
2023
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