Abstract
This research work develops an explicit nonlinear model predictive control strategy for an aerodynamical model i.e. twin rotor MIMO system (TRMS). Here the control strategy is developed by calculating the tracking error as well as the control signal in the prediction horizon using Taylor series expansion. The explicit solution for the control signal is obtained from an optimal performance index which can be developed without online optimization. The complete state information of the system to the proposed controller is given from an ensemble Kalman filter (EnKF) based state observer. The simulation and real-time results are documented in graphical form to confirm the efficiency of the proposed controller.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
