Nonlinear adaptive model following control for a 3-DOF tandem-rotor model helicopter
| Autor: | Mitsuaki Ishitobi, Masatoshi Nishi, Kazuhide Nakasaki |
|---|---|
| Rok vydání: | 2010 |
| Předmět: |
Engineering
Adaptive control Identification scheme Parameter identification Nonlinear control law.invention Computer Science::Robotics Control theory law Electrical and Electronic Engineering Real-time operating system business.industry Applied Mathematics Testbed System identification Control engineering Computer Science Applications Nonlinear system Control and Systems Engineering Model following control Tandem-rotor helicopters Helicopter rotor business |
| Zdroj: | Control Engineering Practice. 18:936-943 |
| ISSN: | 0967-0661 |
| DOI: | 10.1016/j.conengprac.2010.03.017 |
| Popis: | This paper considers two-input, two-output nonlinear adaptive model following control of a 3-DOF (degree-of-freedom) tandem rotor model helicopter. The control performance is studied by real time implementation of the control algorithms in an actual helicopter testbed. Since the decoupling matrix of the model helicopter is singular, the system is not decouplable by static state feedback, and it is challenging to design a feedback control system. Dynamic state feedback is applied. The controller is designed using a nonlinear structure algorithm. Furthermore, a parameter identification scheme is introduced in the closed-loop system to improve the control performance. Three identification methods are discussed. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
|
Full Text from ScienceDirect