Research on finite time control method based on terminal sliding mode for spacecraft attitude
| contributor author | Zheng Yan , Cao Wei | |
| date accessioned | 2020-03-12T20:06:42Z | |
| date available | 2020-03-12T20:06:42Z | |
| date issued | 2014 | |
| identifier other | 6852228.pdf | |
| identifier uri | https://libsearch.um.ac.ir:443/fum/handle/fum/1002263?show=full | |
| format | general | |
| language | English | |
| publisher | IEEE | |
| title | Research on finite time control method based on terminal sliding mode for spacecraft attitude | |
| type | Conference Paper | |
| contenttype | Metadata Only | |
| identifier padid | 8123296 | |
| subject keywords | Heuristics | |
| subject keywords | Machine Scheduling | |
| subject keywords | Optimization Algorithms | |
| subject keywords | Shop Scheduling Problems | |
| identifier doi | 10.1109/ICAICT.2014.7035950 | |
| journal title | ontrol and Decision Conference (2014 CCDC), The 26th Chinese | |
| filesize | 265553 | |
| citations | 0 |
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