A controller design for spacecraft attitude maneuvering with control saturation based on L<inf>2</inf>-gain
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Year
: 2014DOI: 10.1109/AIPR.2014.7041926
Keyword(s): Accuracy,Approximation error,Fourier series,Optimization,Polynomials,Vectors
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A controller design for spacecraft attitude maneuvering with control saturation based on L<inf>2</inf>-gain
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| contributor author | Shi Zhong , Wang Hui , Li Li , Hu Qing-lei | |
| date accessioned | 2020-03-12T20:07:25Z | |
| date available | 2020-03-12T20:07:25Z | |
| date issued | 2014 | |
| identifier other | 6852713.pdf | |
| identifier uri | https://libsearch.um.ac.ir:443/fum/handle/fum/1002740?locale-attribute=en | |
| format | general | |
| language | English | |
| publisher | IEEE | |
| title | A controller design for spacecraft attitude maneuvering with control saturation based on L<inf>2</inf>-gain | |
| type | Conference Paper | |
| contenttype | Metadata Only | |
| identifier padid | 8123837 | |
| subject keywords | Accuracy | |
| subject keywords | Approximation error | |
| subject keywords | Fourier series | |
| subject keywords | Optimization | |
| subject keywords | Polynomials | |
| subject keywords | Vectors | |
| identifier doi | 10.1109/AIPR.2014.7041926 | |
| journal title | ontrol and Decision Conference (2014 CCDC), The 26th Chinese | |
| filesize | 316619 | |
| citations | 1 |