Abstract
This paper describes the experimental estimation of the mini-helicopter inertia and center of gravity (CG) location. A three degree of freedom inertia test rig and an Inertia Measurement Unit (IMU) were used to measure the oscillation frequencies about three axes under different configurations. These frequency data are then manipulated to estimate the inertia tensor and CG location of the mini-helicopter model.
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.
