01.2 - Aircraft Design and Integrated System (Applications)
DESIGN STUDY OF BRAKE MECHANICAL CONTROL SYSTEM OF UAV
J.-J. Leeš, J.-H. Leeš; šKorea Aerospace Research Institute, South Korea
This paper is a study on the linkage design that converts the pedal system of a four-seater aircraft to an unmanned aerial vehicle. It is composed of a four-joint link system and a support structure to enable braking and change of direction using a dual redundant electric actuator. A trade-off study was conducted to optimize the support structure to transmit load properly and four-joint link system to control the angular displacement.