Hardware Design of SUAV Flight Control System Based on STM32F427

DOI

10.2991/csece-18.2018.93How to use a DOI?

Keywords

SUAV; flight control; hardware design; STM32F427

Abstract

As an emerging high-tech device, the SUAV plays a more and more significant role in military and civilian fields because of its advantages such as low cost, high safety, flexible usability and easy maintenance. The flight control system is the core of the SUAV, which exerts a big influence on SUAV performance to a large extent. In order to meet the requirement of low power consumption, simple structure and high performance, this paper designs the hardware of SUAV flight control system based on STM32F427. The modular hardware design is introduced in detail, including the digital control circuit, the power circuit, the sensor circuit and the interface circuit. The flight control system designed in this paper is feasible, effective and reliable, fulfilling the design demand and improving the control and operation performance of the SUAV.

Copyright

© 2018, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Tao Yang
AU  - Liren Chai
AU  - Gang Wang
PY  - 2018/02
DA  - 2018/02
TI  - Hardware Design of SUAV Flight Control System Based on STM32F427
BT  - Proceedings of the 2018 International Conference on Computer Science, Electronics and Communication Engineering (CSECE 2018)
PB  - Atlantis Press
SP  - 435
EP  - 438
SN  - 2352-538X
UR  - https://doi.org/10.2991/csece-18.2018.93
DO  - 10.2991/csece-18.2018.93
ID  - Yang2018/02
ER  -