Hardware System Design of Quad-rotor Aircraft Based on STM32F103
Abstract
The paper outlines the configuration and the hardware system architecture of the quad-rotor aircraft, describes the overall design of the hardware system of the quad-rotor aircraft, expounds the design method of each subsystem of the hardware system of the quad-rotor aircraft, and finally gets the complete hardware system of the quad-rotor aircraft by joining the design results of subsystems.
Keywords
Hardware system, Design, Quad-rotor aircraft, STM32F103.Text
DOI
10.12783/dteees/epme2018/24630
10.12783/dteees/epme2018/24630
Refbacks
- There are currently no refbacks.