Abstract
Pilot induced oscillation of a stable second order system is investigated as an instability that involves the closed loop consisting of the human pilot, the control system and the controlled element.Transfer functions of the human pilot and the control system are assumed. Nondimensionalized closed loop gains on the instability boundary are used as the extent of the instability.Fixed base simulator tests are conducted and the experimental results are compared with the results of theoretical analysis.These results seem to offer good insight into the phenomenon of the pilot induced oscillation.
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.
