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1. 上海交通大学航空航天学院
2. 中国空空导弹研究院
3. 中国人民解放军061基地军事代表室
纸质出版:2011
移动端阅览
曾漫, 熊小丽, 丁文革, 等. 一种典型数字无刷电动舵机的设计[J]. 中北大学学报(自然科学版), 2011,32(6):751-757.
曾漫, 熊小丽, 丁文革, et al. Design of a Typical Digital Brushless Electric Steering Engine[J]. 2011, 32(6): 751-757.
为满足新型空空导弹高机动性、快速性的要求
基于DSP设计了一种典型数字无刷电动舵机系统.首先分析了数字无刷电动舵机的组成与功能
并从传动机构、反馈装置、控制电路、舵面锁制器、控制算法、控制软件和舵机自检等各主要组成部分
对舵机系统的性能参数设计进行了分析和阐述.实验结果表明
数字无刷电动舵机系统最大负载扭矩为75 N.m
空载角速度为600°/s
满载角速度为200°/s
动态相移为28°(1°
20 Hz).该系统在提高控制精度的同时
较传统模拟电动舵机具有深度自检功能
实现了全弹的数字化.经适应性优化
可完成更复杂控制算法如变结构控制
模糊控制的设计实现.
A new DSP-based digital brushless electric steering engine system was designed to meet the requirements of high maneuverability and rapid response of the up-to-date air to air missiles.The composition and function of the steering engine were analyzed.The performance parameters were analyzed and described with regard to main components
including transmission mechanism
feedback devices
control circuits
steering engine lock
control algorithms
control software and steering engine self-test.The experiment results showed that the engine system features max.loading torque of 75 N·m
idle angular speed of 600 °/ s
full-load angular speed of 200 °/s
dynamic phase shift of 28°(20 Hz
1° as amplitude).Equipped with deep self-test function and full digitalization units
the engine system has better control accuracy than the traditionally used analog one.Through adaptive optimization
the system will open to much more complex control algorithms such as variable structure control and fuzzy control.
崇阳,李言俊,张科,等.基于DSP的模糊PID舵机控制算法设计与实现[J].飞行力学,2011,29(2):86-88.Chong Yang,Li Yanjun,Zhang Ke,et al.Design and implementation of digital fuzzy-PID actuator control system[J].Flight Dynamics,2011,29(2):86-88.(in Chinese)
周小庆,李平,韩波.基于DSP前馈模糊PI的舵机控制算法[J].计算机工程,2010,36(14):209-211.Zhou Xiaoqing,Li Ping,Han Bo.Servo actuator control algorithm based on feedforward fuzzy PI of DSP[J].Computer Engineering,2010,36(14):209-211.(in Chinese)
袁媛,王忠庆,秦彬.基于DSP无人飞行器数字舵机控制仪研究[J].电气技术,2010(2):41-43.Yuan Yuan,Wang Zhongqing,Qin Bin.Research of digital servo controller unmanned aerial vehicle based on DSP[J].Electrical Engineering,2010(2):41-43.(in Chinese)
李赛辉,雷金奎.基于DSP的数字舵机控制系统的设计与实现[J].计算机测量与控制,2009,17(3):484-486.Li Saihui,Lei Jinkui.Design and implementation of digital rudder control system based on DSP[J].ComputerMeasurement and Control,2009,17(3):484-486.(in Chinese)
梁晓庚,王伯荣,余志峰,等.空空导弹制导控制系统设计[M].北京:国防工业出版社,2006.
郑浩鑫,郑宾,李建民.基于TMS320F2812无刷直流电机控制系统设计[J].国外电子元器件,2008(11):17-19.Zheng Haoxin,Zheng Bin,Li Jianmin.Design of control system of brushless DC motor based on TMS320F2812[J].International Electronic Elements,2008(11):17-19.(in Chinese)
刘涛,吕迅,黄一敏.基于DSP的数字舵机控制器设计[J].沈阳航空工业学院学报,2006,23(1):8-11.Liu Tao,LüXunhong,Huang Yimin.The design of numeric rudder controller base on DSP[J].Journal of ShenyangInstitute of Aeronautical Engineering,2006,23(1):8-11.(in Chinese)
邓煜坤.单相磁滞电动机机械特性研究[J].微电机,2006,39(8):34-37.Deng Yukun.Resarch for machine torque of the hysteresis motor[J].Micromotors,2006,39(8):34-37.(inChinese)
高同跃,龚振邦,罗均,等.一种超小型无人机舵机控制系统的设计[J].计算机测量与控制,2007,15(8):1006-1007.Gao Tongyue,Gong Zhengbang,Luo Jun,et al.Servo controller design based on C8051F121 for small unmannedaerial vehicle[J].Computer Measurement&Control,2007,15(8):1006-1007.(in Chinese)
魏林,陈欣,吕迅.无人机舵回路伺服系统变阻尼控制律研究[J].电气传动,2008,38(10):51-53.Wei Lin,Chen Xin,LüXunhong.Research of changeable damping control law in a rudder loop servo system forUAV[J].Electric Drive,2008,38(10):51-53.(in Chinese)
苏永振,胡延霖,赵菲,等.基于ARM的无人机飞行控制系统的实现[J].计算机测量与控制,2005,13(10):1063-1065.Su Yongzhen,Hu Yanlin,Zhao Fei,et al.Design of the hardware of a UAV flight control system based on ARM[J].Computer Measurement&Control,2005,13(10):1063-1065.(in Chinese)
刘和平.TMS320LF240X DSP C语言开发应用[M].北京:北京航空航天大学出版社,2003.
刘歌群,卢京潮,闫建国,等.用单片机产生7路舵机控制PWM波的方法[J].机械与电子,2004(2):76-78.Liu Gequn,Lu Jingchao,Yan Jianguo,et al.Method to generate 7 pulse-width modulation waves with single-chipmicroprocessor to control servos[J].Machiner-y&Electronics,2004(2):76-78.(in Chinese)
何卫国,彭科容.一种小型空空导弹舵面锁制器的设计实现[J].科技咨询,2009(20):94.He Weiguo,Peng Kerong.A small rudder surface to air missile system design and implementation of the lock[J].Science&Technology Information,2009(20):94.(in Chinese)
王晔.直流无刷舵机控制策略研究[D].河南:河南科技大学,2008.
魏林,陈欣,吕迅.无人机无刷直流数字式舵机控制器设计[J].微电机,2008,41(5):46-48.Wei Lin,Chen Xin,LüXunhong.Design of brushless direct current numerical rudder controller for UAV[J].Micromotors,2008,41(5):46-48.(in Chinese)
邱建东,胡永红.无人机数据链自动测试系统测控组件的设计[J].计算机测量与控制.2006,14(1):7-9.Qiu Jiandong,Hu Yonghong.Design of the test&control subassembly of the automatic test system for data link ofUAV[J].Computer Measurement&Control,2006,14(1):7-9.(in Chinese)
Chou C P,Hannafordb.Measurement and modeling of mckibben pneurnatic artificial muscle[J].IEEETransactions on Robotics and Automation,1996,12(1):90-102.
Gentan.Engineering with rubber:how to design-rubber components[M].Munich:Hanser Publisher,2001.
刘昆朋,曾庆华.导弹舵机参数故障诊断方法[J].导弹与航天运载技术,2008(6):13-16.Liu Kunpeng,Zeng Qinghua.Fault diagnosis method for missile electromechanical actuator[J].Missile and SpaceVehcil,2008(6):13-16.(in Chinese)
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