Abstract
Fuzzy logic control of longitudinal motion of an aircraft based on Takagi–Sugeno modelling approach is presented in this paper. Takagi–Sugeno model of the motion along the desired trajectory is used for state-space parallel decomposition controller (PDC) design. The proposed control scheme guarantees stability of closed loop and asymptotical step pitch angle reference signal tracking. Simulation results on twin-engine short-range transport aircraft LET L410 indicate that the proposed control law can represent a feasible aircraft motion control technique and especially in presence of model inaccuracies and disturbances it overcomes the most commonly used approaches.
Sign-in/Register to access full text options 
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.
