Design of micro UAV flight control system based on SOPC

SONG Yu; SONG Jun-wei

doi:10.13873/J.1000-9787(2016)09-0101-03

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Design of micro UAV flight control system based on SOPC

更新时间：2025-09-11

- Design of micro UAV flight control system based on SOPC
- Vol. 35, Issue 9, Pages: 101-103(2016)
- 作者机构：
  
  长春工业大学计算机科学与工程学院
- 作者简介：
- 基金信息：
- DOI：10.13873/J.1000-9787(2016)09-0101-03
  CLC： V279;V249.1
- Published：2016
- 稿件说明：
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[1]宋宇,宋隽炜.基于SOPC的微型无人机飞行控制系统设计[J].传感器与微系统,2016,35(09):101-103.

SONG Yu, SONG Jun-wei. Design of micro UAV flight control system based on SOPC[J]. 2016, 35(9): 101-103.
[1]宋宇,宋隽炜.基于SOPC的微型无人机飞行控制系统设计[J].传感器与微系统,2016,35(09):101-103. DOI： 10.13873/J.1000-9787(2016)09-0101-03.

SONG Yu, SONG Jun-wei. Design of micro UAV flight control system based on SOPC[J]. 2016, 35(9): 101-103. DOI： 10.13873/J.1000-9787(2016)09-0101-03.

摘要

针对无人机（UAV）飞控系统的发展要求

提出了一种基于可编程片上系统（SOPC）技术的设计方案

自顶向下地利用软硬件协同设计方法实现整个过程的设计。主控芯片采用Cyclone II系列的EP2C8Q208C8N

进而设计系统的外围电路;借助NIOS II软件写入程序实现对无人机的控制。与传统的无人机控制系统相比

该系统适应了集成度高、功耗低、体积小的发展要求。悬停试飞

机体晃动小

且在外界干扰时能自动调整姿态

保持稳定飞行

具有较快的响应速度。

Abstract

Aiming at demand for development of unmanned aerial vehicle（UAV） flight control system

propose a design scheme based on SOPC technology.By using method of collaborative design of software and hardware

realize design of whole process from top to down.Use Cyclone II EP2C8Q208C8 N as main control chip

and then design peripheral circuit of system.By writing procedures with NIOS II software to achieve control of the UAV.Compared with conventional UAV control system

the system adapts to development requirements of high integration

low power consumption

small size.Its body shakes slightly during hover flight and it can automatically adjust attitude and flight stably with a fast response when there is outside interference.

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references

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