Control Law Design for Twin Rotor MIMO System with Nonlinear Control Strategy
Modeling of complex air vehicles is a challenging task due to high nonlinear behavior and significant coupling effect between rotors. Twin rotor multi-input multioutput system (TRMS) is a laboratory setup designed for control experiments, which resembles a helicopter with unstable, nonlinear, and co...
Saved in:
| Main Authors: | , , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2016-01-01
|
| Series: | Discrete Dynamics in Nature and Society |
| Online Access: | http://dx.doi.org/10.1155/2016/2952738 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832563474986696704 |
|---|---|
| author | M. Ilyas N. Abbas M. UbaidUllah Waqas A. Imtiaz M. A. Q. Shah K. Mahmood |
| author_facet | M. Ilyas N. Abbas M. UbaidUllah Waqas A. Imtiaz M. A. Q. Shah K. Mahmood |
| author_sort | M. Ilyas |
| collection | DOAJ |
| description | Modeling of complex air vehicles is a challenging task due to high nonlinear behavior and significant coupling effect between rotors. Twin rotor multi-input multioutput system (TRMS) is a laboratory setup designed for control experiments, which resembles a helicopter with unstable, nonlinear, and coupled dynamics. This paper focuses on the design and analysis of sliding mode control (SMC) and backstepping controller for pitch and yaw angle control of main and tail rotor of the TRMS under parametric uncertainty. The proposed control strategy with SMC and backstepping achieves all mentioned limitations of TRMS. Result analysis of SMC and backstepping control schemes elucidates that backstepping provides efficient behavior with the parametric uncertainty for twin rotor system. Chattering and oscillating behaviors of SMC are removed with the backstepping control scheme considering the pitch and yaw angle for TRMS. |
| format | Article |
| id | doaj-art-149a99d67c4848188f6775695bdbf003 |
| institution | Kabale University |
| issn | 1026-0226 1607-887X |
| language | English |
| publishDate | 2016-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Discrete Dynamics in Nature and Society |
| spelling | doaj-art-149a99d67c4848188f6775695bdbf0032025-02-03T01:20:04ZengWileyDiscrete Dynamics in Nature and Society1026-02261607-887X2016-01-01201610.1155/2016/29527382952738Control Law Design for Twin Rotor MIMO System with Nonlinear Control StrategyM. Ilyas0N. Abbas1M. UbaidUllah2Waqas A. Imtiaz3M. A. Q. Shah4K. Mahmood5Department of Electrical Engineering, Iqra National University, Peshawar 25000, PakistanDepartment of Electrical Engineering, CIIT, Islamabad 45550, PakistanDepartment of Electrical Engineering, CIIT, Islamabad 45550, PakistanDepartment of Electrical Engineering, Iqra National University, Peshawar 25000, PakistanDepartment of Electrical Engineering, CIIT, Islamabad 45550, PakistanDepartment of Electrical Engineering, Iqra National University, Peshawar 25000, PakistanModeling of complex air vehicles is a challenging task due to high nonlinear behavior and significant coupling effect between rotors. Twin rotor multi-input multioutput system (TRMS) is a laboratory setup designed for control experiments, which resembles a helicopter with unstable, nonlinear, and coupled dynamics. This paper focuses on the design and analysis of sliding mode control (SMC) and backstepping controller for pitch and yaw angle control of main and tail rotor of the TRMS under parametric uncertainty. The proposed control strategy with SMC and backstepping achieves all mentioned limitations of TRMS. Result analysis of SMC and backstepping control schemes elucidates that backstepping provides efficient behavior with the parametric uncertainty for twin rotor system. Chattering and oscillating behaviors of SMC are removed with the backstepping control scheme considering the pitch and yaw angle for TRMS.http://dx.doi.org/10.1155/2016/2952738 |
| spellingShingle | M. Ilyas N. Abbas M. UbaidUllah Waqas A. Imtiaz M. A. Q. Shah K. Mahmood Control Law Design for Twin Rotor MIMO System with Nonlinear Control Strategy Discrete Dynamics in Nature and Society |
| title | Control Law Design for Twin Rotor MIMO System with Nonlinear Control Strategy |
| title_full | Control Law Design for Twin Rotor MIMO System with Nonlinear Control Strategy |
| title_fullStr | Control Law Design for Twin Rotor MIMO System with Nonlinear Control Strategy |
| title_full_unstemmed | Control Law Design for Twin Rotor MIMO System with Nonlinear Control Strategy |
| title_short | Control Law Design for Twin Rotor MIMO System with Nonlinear Control Strategy |
| title_sort | control law design for twin rotor mimo system with nonlinear control strategy |
| url | http://dx.doi.org/10.1155/2016/2952738 |
| work_keys_str_mv | AT milyas controllawdesignfortwinrotormimosystemwithnonlinearcontrolstrategy AT nabbas controllawdesignfortwinrotormimosystemwithnonlinearcontrolstrategy AT mubaidullah controllawdesignfortwinrotormimosystemwithnonlinearcontrolstrategy AT waqasaimtiaz controllawdesignfortwinrotormimosystemwithnonlinearcontrolstrategy AT maqshah controllawdesignfortwinrotormimosystemwithnonlinearcontrolstrategy AT kmahmood controllawdesignfortwinrotormimosystemwithnonlinearcontrolstrategy |