Abstract
Purpose: This article proposes a chattering-free sliding mode control scheme with unidirectional auxiliary surfaces (UAS-SMC) for small miniature autonomous helicopters (Trex 250). Design/methodology/approach: The proposed UAS-SMC scheme consists of a nested sequence of rotor dynamics, angular rate, Euler angle, velocity and position loops. Findings: It is demonstrated that the UAS-SMC strategy can eliminate the chattering phenomenon exhibiting in the convenient SMC method and achieve a better approaching speed. Originality/value: The proposed control strategy is implemented on the helicopter and flight tests clearly demonstrate that a much better performance could be achieved, compared with convenient SMC schemes.
Original language | English |
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Pages (from-to) | 421-438 |
Number of pages | 18 |
Journal | International Journal of Intelligent Computing and Cybernetics |
Volume | 5 |
Issue number | 3 |
DOIs | |
Publication status | Published - Aug 2012 |
Keywords
- Approaching speed
- Chattering
- Flight control
- Helicopters
- Sliding mode control
- Unmanned aircraft
ASJC Scopus subject areas
- General Computer Science