Adaptive control of a position servo as a first stage in fatigue investigation
An aircraft will encounter various forces and pressures applied by the air to its structure during flight. Therefore static and dynamic fatigue testing are necessary to make sure its structure can stand various force pattern imposed on it. In this study, a dc servo was configured for position contro...
| Main Authors: | , |
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| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
Universiti Putra Malaysia Press
2002
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| Online Access: | http://psasir.upm.edu.my/id/eprint/18382/1/18382.pdf |