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计算机工程 ›› 2009, Vol. 35 ›› Issue (16): 237-239. doi: 10.3969/j.issn.1000-3428.2009.16.085

• 工程应用技术与实现 • 上一篇    下一篇

小型低空飞艇中的舵机控制系统

施兴祖1,刘世前2,敬忠良2   

  1. (1. 上海交通大学电子信息与电气工程学院,上海 200240;2. 上海交通大学空天科学技术研究院,上海 200240)
  • 收稿日期:1900-01-01 修回日期:1900-01-01 出版日期:2009-08-20 发布日期:2009-08-20

Servo Control System in Small Low Altitude Airship

SHI Xing-zu1, LIU Shi-qian2, JING Zhong-liang2   

  1. (1. School of Electronic Information & Electrical Engineering, Shanghai Jiaotong University, Shanghai 200240;2. Institute of Aerospace Science & Technology, Shanghai Jiaotong University, Shanghai 200240)
  • Received:1900-01-01 Revised:1900-01-01 Online:2009-08-20 Published:2009-08-20

摘要: 为满足小型低空验证飞艇的舵机控制需求,研究并设计以MSP430F149单片机为核心处理器的舵机控制系统,介绍其硬件结构及软件流程,并在基于PID控制策略的闭环仿真平台上加以实现。实验结果表明,该系统功耗低、结构紧凑、抗干扰能力强,具有良好的跟踪性能。

关键词: 飞艇, 帧协议, 闭环

Abstract: In order to meet the requirements of servo control in small low altitude verifying airship, a servo control system is researched and designed, which uses MSP430F149 singlechip as its core processor. The hardware frame and software flow are introduced. It is implemented on closed loop simulation platform based on PID control strategy. Experimental results show this system has some merits such as low power consumption, compact conformation, and strong capacity of resisting disturbance, it has better performance of tracking.

Key words: airship, frame protocol, closed loop

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