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Improved integral backstepping control of variable speed motion systems with application to a laboratory helicopter
A Haruna1, Z Mohamed2, M Ö Efe3
1School of Electrical Engineering, Universiti Teknologi Malaysia, 81310 UTM, Johor Bahru, Johor, Malaysia; Department of Mechatronics Engineering Bayero University Kano, Nigeria.
This study introduces an enhanced integral backstepping control for the Two-Rotor Aero-dynamic System (TRAS), improving transient response and tracking performance. The method demonstrates robustness against system coupling and external disturbances like wind gusts.
Area of Science:
- Robotics and Control Systems
- Aerospace Engineering
- Nonlinear Control Theory
Background:
- The Two-Rotor Aero-dynamic System (TRAS) presents complex nonlinear dynamics and coupling effects, posing challenges for precise real-time control.
- Existing control methods often struggle with improving transient response and tracking accuracy, especially under external disturbances.
- Integral backstepping is a powerful technique for nonlinear systems, but its application to systems like TRAS requires enhancements.
Purpose of the Study:
- To develop an improved integral backstepping control strategy for the TRAS.
- To enhance the transient response and tracking performance for both constant and time-varying references.
- To validate the proposed method's robustness against system coupling and external disturbances.
Main Methods:
- Decomposition of the TRAS into horizontal (HS) and vertical (VS) subsystems.
- Augmentation of traditional backstepping with direct integral action for each subsystem.
- Modification of the dual boundary conditional integration method to improve transient response.
- Implementation of a switching technique to address jerking effects in the HS bi-directional motor.
Main Results:
- The proposed integral backstepping method significantly improved transient and tracking performance compared to prior conditional integration techniques.
- Experimental results confirmed enhanced performance for both constant and time-varying reference tracking.
- The control strategy demonstrated robustness against inherent system coupling and simulated wind gust disturbances.
Conclusions:
- The enhanced integral backstepping approach offers superior real-time control for the TRAS.
- The modified dual boundary conditional integration and switching technique effectively address system nonlinearities and disturbances.
- This method provides a robust and high-performance solution for controlling complex aerial robotic systems.
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