Abstract
A simplified but comprehensive model for helicopter and external suspended load, based on the linear superposition of effects, is defined. The coherence of the external load modal response and of the helicopter response to control input is verified through available reference data. Finally, the impact of the slung load on the overall system dynamic stability, on the helicopter response to control input, and on flight qualities is assessed.
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.
