Abstract
The 3-DOF four rotors system is a typical high-order, nonlinear, multi-variable and strong coupling complex system. The motion equations of the yaw, pitch and roll axes can simulate the flight characteristics of the actual helicopter. It is usually difficult to establish the accurate mathematical model for the influence of the parameter perturbation and the external disturbance. According to this instance, the mixed sensitivity robust control method is proposed to improve the system control qualities. The simulation results shown that the controller can make the 3-DOF helicopter system have good robust stability and dynamic performance when the model object parameters exist uncertainty.
Original language | English |
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Title of host publication | Proceedings - 2012 5th International Symposium on Computational Intelligence and Design, ISCID 2012 |
Pages | 306-309 |
Number of pages | 4 |
DOIs | |
Publication status | Published - 2012 |
Event | 2012 5th International Symposium on Computational Intelligence and Design, ISCID 2012 - Hangzhou, China Duration: 28 Oct 2012 → 29 Oct 2012 |
Publication series
Name | Proceedings - 2012 5th International Symposium on Computational Intelligence and Design, ISCID 2012 |
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Volume | 1 |
Conference
Conference | 2012 5th International Symposium on Computational Intelligence and Design, ISCID 2012 |
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Country/Territory | China |
City | Hangzhou |
Period | 28/10/12 → 29/10/12 |
Keywords
- 3-DOF helicopter
- Four rotors
- Mixed sensitivity
- Robust control