Abstract
This survey presents the application of force feedback in aviation. In modern fly-by-wire control system, actuator rate limit is the primary source of PIO II (Pilot Induced Oscillation II). The combination of smart-cue and smart-gain method can alleviate PIO II effectively, and consequently enhance the flight safety. The recent research of applying force feedback in aviation demonstrates that it is worthy of theoretical exploration and extensive utilization.
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.
