Autopilot Design and Reseach of MiniPilot2812

DING  Hongjun; WANG  Xibin; LIU  Zhiqiang; ZANG  Jisong

doi:10.15892/j.cnki.djzdxb.2010.01.008

Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 1: 62 - 64

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.01.008

MISSILES AND GUIDANCE TECHNOLOGY

Autopilot Design and Reseach of MiniPilot2812

DING Hongjun ,
WANG Xibin ,
LIU Zhiqiang ,
ZANG Jisong

Expand

¹ School of Mechanical and Vehicular Engineering, Beijing Institute and Technology, Beijing 100081,China
² North China Institute of Aerospace Engineering, Hebei Langfang 065000, China

Received date: 2008-12-29

Online published: 2025-05-19

Fold

Abstract

This paper presents an autopilot design and research of MiniPilot2812 base on two T MS320F2812 for controlling computer and navigation computer. The autopilot adopt control model of PID to stabilize and operate UAV, adopt the integrated navigation of GPS/INS and realize real-time control and adjustment by wireless data transmission and the information communication of ground station; MiniPilot2812 autopilot meet the base flight demand after many trial run and flight tests.

Key words： autopilot; TMS320F2812; hardware design; software design; integrated navigation

Cite this article

DING Hongjun , WANG Xibin , LIU Zhiqiang , ZANG Jisong . Autopilot Design and Reseach of MiniPilot2812[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(1) : 62 -64 . DOI: 10.15892/j.cnki.djzdxb.2010.01.008

References

[1]	张明廉. 飞行控制系统[M]. 北京: 航空工业出版社, 1984.
[2]	薛尧舜. 无人机控制器软件与控制算法研究[D]. 西安: 西北工业大学, 2003.
[3]	鲁道夫·布罗克豪斯. 飞行控制[M]. 北京: 国防工业出版社, 1999.
[4]	杨华保, 何子华, 田宏星. 一种小型自主飞行无人机系统集成设计研究[J]. 航空计算技术, 2007, 31(02): 11- 13.
[5]	刘歌群. 无人机飞行控制器设计及检测与控制技术研究[D]. 西安: 西北工业大学, 2004.
[6]	王晓文, 王浚. 飞机环境控制系统并行设计[J]. 北京航空航天大学学报, 2003, 5(22): 21- 23.

Options

Outlines

模态框（Modal）标题

Abstract

Cite this article

References