Adaptive Synergetic Controller for Stabilizing the Altitude and Angle of Mini Helicopter. | [Mehran University Research Journal of Engineering and Technology • 2019]

Author(s):

1. Zain Anwar Ali: School of Automation Engineering, South East University, Nanjing, Jiangsu, China

2. LI XINDE: School of Automation Engineering, South East University, Nanjing, Jiangsu, China

Abstract:

This research proposes ASC (Adaptive Synergetic Controller) for the nonlinear model of MH (Mini Helicopter) to stabilize the desired altitude and angle. The model of MH is highly nonlinear, underactuated and multivariable in nature due to its dynamic uncertainties and restrictions of velocities during the flight. ASC can force the tracking errors of the system states converges to zero in a finite interval of time. The MH system requires smooth controller and fast precise transition response from initial state till the desired state, therefore the parametric calculations and simulations can be done by the proposed ASC algorithm. It is validated that the above simulated results of the proposed controller have a better convergence rate and smoother stability response in order to track the desired altitude and angle when compared with SMC (Sliding Mode Controller). Moreover, it does not need any linearization, transformation and variations in the system model.

Page(s): 251-258

DOI: 10.22581/muet1982.1902.01

Published: Journal: Mehran University Research Journal of Engineering and Technology, Volume: 38, Issue: 2, Year: 2019

Keywords:

Keywords are not available for this article.

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