Abstract
This paper deals with the design of low order controllers for the tactical transport UH 60 Black Hawk helicopter. Two low order H∞ loop shaping control design techniques, which are amendable to Linear matrix Inequalities, are presented and discussed. The first synthesis implements a cone-complementarity algorithm while the second method exploits sufficient conditions in the H∞ problem leading to a simple, non-iterative control synthesis procedure. The validity of these control techniques are compared and demonstrated both in terms of computational efficiency and control performance achieved through a linearized model of the UH 60 helicopter.
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.
