Title :
The dynamics research on the composite undercarriage of the Unmanned Aerial Vehicle
Author :
Yu-xiu Hou ; Yong-liang Guan ; Hong-guang Jia ; Liu Bo ; Wu-Yuan Ma
Author_Institution :
Changchun Univ. of Sci. & Technol., Changchun, China
Abstract :
The Undercarriage is affected by the dynamic load when the Unmanned Aerial Vehicle (UAV) taxis and lands on the ground, especially during the landing to the ground, it needs higher requirements. The dynamical deformation and strength characteristics of the Undercarriage directly determine its performance and affect the safety of the UAV. In the article, we study the dynamical deformation, the strength calculation and the experiments in order to understand whether it can meet the requirements of design and use or not. By the strength check of Tsai-Wu strength theory and ultrasonic flaw detection technology, the strength of the landing gears meets the needs of UAV.
Keywords :
autonomous aerial vehicles; design engineering; gears; robot dynamics; Tsai-Wu strength theory; UAV; composite undercarriage; dynamic load; dynamical deformation; landing gears; ultrasonic flaw detection technology; unmanned aerial vehicle; Atmospheric modeling; Carbon; Finite element analysis; Glass; Software; Springs; Vehicle dynamics; Composites Undercarriage Dynamics;
Conference_Titel :
Mechatronics and Automation (ICMA), 2015 IEEE International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4799-7097-1
DOI :
10.1109/ICMA.2015.7237480