| Reference Type | Journal (article/letter/editorial) |
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| Title | Fault-Tolerant Attitude Control System for a Spacecraft with Control Moment Gyros Using Multi-Objective Optimization |
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| Journal | International Journal of Advanced Computer Science and Applications |
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| Authors | Noumi, Ai | Author |
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| Misuzu, Haruki | Author |
| Kanzawa, Takuya | Author |
| Takahashi, Masaki | Author |
| Year | 2015 | Volume | 6 |
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| Publisher | The Science and Information Organization |
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| DOI | doi:10.14569/ijacsa.2015.060106Search in ResearchGate |
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| Generate Citation Formats |
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| Mindat Ref. ID | 10369972 | Long-form Identifier | mindat:1:5:10369972:3 |
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|
| GUID | 0 |
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| Full Reference | Noumi, Ai, Misuzu, Haruki, Kanzawa, Takuya, Takahashi, Masaki (2015) Fault-Tolerant Attitude Control System for a Spacecraft with Control Moment Gyros Using Multi-Objective Optimization. International Journal of Advanced Computer Science and Applications, 6. doi:10.14569/ijacsa.2015.060106 |
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| Plain Text | Noumi, Ai, Misuzu, Haruki, Kanzawa, Takuya, Takahashi, Masaki (2015) Fault-Tolerant Attitude Control System for a Spacecraft with Control Moment Gyros Using Multi-Objective Optimization. International Journal of Advanced Computer Science and Applications, 6. doi:10.14569/ijacsa.2015.060106 |
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| In | (n.d.) International Journal of Advanced Computer Science and Applications Vol. 6. The Science and Information Organization |
|---|
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