Identification and control of a small-scale helicopter
Designing reliable flight control for an autonomous helicopter requires a high performance dynamics model. In this paper, a nonlinear autoregressive with exogenous inputs (NLARX) model is selected as the mathematical structure for identifying and controlling the flight of a small-scale helicopter. A...
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| Main Authors: | , |
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| Format: | Article |
| Published: |
Springer Verlag (Germany)
2010
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| Subjects: | |
| Online Access: | http://eprints.um.edu.my/11891/ |
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| Institution: | Universiti Malaya |
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