Abstract
Structural damage brings strong coupling effects and increases the difficulty of flight control. Aiming at this problem, a nonlinear model of aircraft is introduced firstly, and then an adaptive non-singular terminal sliding mode control method is presented. The approach can ensure the system to reach the sliding surface and converge to equilibrium point in finite time from any initial state without the singularity. In addition, the proposed adaptive non-singular terminal sliding mode controller can real-time estimate the uncertainties and external disturbances. The adaptive law is derived in the Lyapunov framework, which can guarantee the asymptotical stability of the closed loop system. Finally, simulations with Generic Transport Model (GTM) are conducted to demonstrate the effectiveness and advantages of the proposed approach.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: 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.