Abstract
A three-time-scale singular perturbation control law is designed for a nonlinear helicopter model in vertical flight. The proposed control law is based on time-scale decomposition, and is able to achieve the desired altitude by selecting a desired angular velocity, and the associated collective pitch angle of the blades. Numerical results for the singular perturbation control strategy, along with comparison results with the literature, are also presented for the studied nonlinear highly coupled helicopter model.
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.
