Sliding Mode Implementation of an Attitude Command Flight Control System for a Helicopter in Hover
This paper presents an investigation into the design of a flight control system, using a decoupled non-linear sliding mode control structure, designed using a linearised, 9th order representation of the dynamics of a PUMA helicopter in hover. The controllers are then tested upon a higher order, non-...
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| Hlavní autoři: | , , |
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| Médium: | Artigo |
| Jazyk: | Inglês |
| Vydáno: |
CTU Central Library
2005-01-01
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| Edice: | Acta Polytechnica |
| Témata: | |
| On-line přístup: | https://ojs.cvut.cz/ojs/index.php/ap/article/view/748 |
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