Integral-type sliding mode fault-tolerant control for attitude stabilization of spacecraft
Two fault-tolerant control (FTC) schemes for spacecraft attitude stabilization with external disturbances are proposed in this brief. The approach is based on integral-type sliding mode control strategy to compensate for actuator faults without controller reconfiguration. First, a basic integral-typ...
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| Main Authors: | , , , |
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| Other Authors: | |
| Format: | Article |
| Language: | English |
| Published: |
2015
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| Online Access: | https://hdl.handle.net/10356/79311 http://hdl.handle.net/10220/38578 |
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| Institution: | Nanyang Technological University |
| Language: | English |