Peak-to-average ratio suppression technology of aerospace tension servo mechanism
-
摘要:
系绳张力的建立需要收绳与目标物拖曳之间存在速度差,针对传统PI控制难以在张力建立或释放等动态过程中获得平稳快速的控制效果问题,提出了一种将积分控制器分段组合的抗冲击策略,在张力建立过程中采用纯积分控制,当张力反馈接近参考值时,加入比例控制使张力值快速收敛,进而较为精确地建立张力,并有效抑制张力冲击,同时采用积分重置的方法使动态控制过程前后张力连续稳定。仿真和样机实验表明,该控制策略精度较高,张力突变过程响应平稳且迅速,且不需要引入额外的物理量,结构简单,占用硬件资源少,可靠性较高。
-
关键词:
- 柔性伺服 /
- 永磁电动机 /
- 张力控制 /
- 抗冲击策略 /
- 比列-积分-微分控制(PID)
Abstract:Establishment of the tether tension requires a speed difference between the rope retraction and the target drag, making it difficult for the traditional PI control to obtain a stable and fast control effect in the dynamic process of tension establishment or release. To solve the problem, an anti-impact strategy was proposed, in which integral controllers were piecewise combined. Only integral control was used in the process of tension establishment. When the tension feedback was close to the reference value, the proportional control was added to make the tension value converge quickly, then the tension was established more accurately and the tension impact was effectively suppressed. Meanwhile, the integral reset method was used to make the tension continuous and stable before and after the dynamic control process. Simulation and prototype experiments showed that the anti-impact control strategy had high accuracy, and the response to tension sudden changes was smooth and rapid. At the same time, the control strategy did not need to introduce additional physical quantities, featuring simple structure and high reliability, and occupying less hardware resources.
-
表 1 永磁同步电动机柔性系绳张力控制系统主要参数
Table 1. Main parameters of flexible tether tension control system based on permanent magnet synchronous motor
参数 数值 夹送电动机(A) 收卷电动机(B) 系绳弹性系数/(N/m) 140 系绳速度变化范围/(m/s) 0~0.5 母线电压/V 28.0 28.0 额定转速/(r/min) 1100 1100 额定转矩/(mN·m) 50 200 额定电流/A 0.35 1.3 最大转矩/(mN·m) 150 400 最大转矩速度/(r/min) 400 400 相电阻/Ω 11.5 3.6 相电感/mH 4.78 3.86 极对数 6 5 -
[1] 黄玉平,崔佩娟,安林雪,等. 高品质航天伺服产品及其实现途径探索[J]. 导弹与航天运载技术(中英文),2022(6): 38-42.HUANG Yuping,CUI Peijuan,AN Linxue,et al. High-quality aerospace servo products and its realization way to explore[J]. Missiles and Space Vehicles,2022(6): 38-42. (in Chinese) [2] 杨雷,张柏楠,郭斌,等. 新一代多用途载人飞船概念研究[J]. 航空学报,2015,36(3): 703-713.YANG Lei,ZHANG Bainan,GUO Bin,et al. Concept definition of new-generation multi-purpose manned spacecraft[J]. Acta Aeronautica et Astronautica Sinica,2015,36(3): 703-713. (in Chinese) [3] 喻思琪,张小红,郭斐,等. 卫星导航进近技术进展[J]. 航空学报,2019,40(3): 022200.YU Siqi,ZHANG Xiaohong,GUO Fei,et al. Recent advances in precision approach based on GNSS[J]. Acta Aeronautica et Astronautica Sinica,2019,40(3): 022200. (in Chinese) [4] 李小彭,尚东阳,陈仁桢,等. 基于机械臂位姿变换的柔性负载伺服驱动系统控制策略[J]. 机械工程学报,2020,56(21): 56-69. doi: 10.3901/JME.2020.21.056LI Xiaopeng,SHANG Dongyang,CHEN Renzhen,et al. Control strategy of flexible load servo drive system based on manipulator position and position transformation[J]. Journal of Mechanical Engineering,2020,56(21): 56-69. (in Chinese) doi: 10.3901/JME.2020.21.056 [5] 钟靖龙,宋宝,刘永兴,等. 基于DDPG的柔性伺服系统级联陷波器设计[J]. 微电机,2022,55(5): 40-44, 61.ZHONG Jinglong,SONG Bao,LIU Yongxing,et al. Deep deterministic policy gradient-based design of cascade notch filters for suppressing mechanical resonance in flexible servo system[J]. Micromotors,2022,55(5): 40-44, 61. (in Chinese) [6] 刘凯宁. 机器人柔性臂伺服系统振动抑制研究[D]. 哈尔滨: 哈尔滨工业大学, 2021.LIU Kaining. Research on vibration suppression of flexible manipulator servo system[D]. Harbin: Harbin Institute of Technology, 2021. (in Chinese) [7] 王云周. 基于CMAC控制策略柔性联接电液位置伺服系统特性研究[D]. 哈尔滨: 哈尔滨理工大学, 2020.WANG Yunzhou. Research on characteristics of flexible linked electro-hydraulic position servo system based on CMAC control strategy[D]. Harbin: Harbin University of Science and Technology, 2020. (in Chinese) [8] BISCHOF B,KERSTEIN L. ROGER-robotic geostationary orbit restorer[J]. Science and Technology Series,2004,109: 183-193. [9] BROPHY J R, FRIEDMAN L, CULICK F. Asteroid retrieval feasibility[C]//2012 IEEE Aerospace Conference. Piscataway, US: IEEE, 2012: 1-16. [10] BRPPHY J R, MUIRHEAD B. Near-earth asteroid retrieval mission (ARM) study[R]. Washington DC: The 33rd International Electric Propulsion Conference, 2013. [11] NAKASUKA S,FUNASE R,NAKADA K,et al. Large membrane “Furoshiki Satellite” applied to phased array antenna and its sounding rocket experiment[J]. Acta Astronautica,2006,58(8): 395-400. doi: 10.1016/j.actaastro.2005.12.010 [12] FANG Z J,ZHANG H J,SHAO C Y,et al. Control strategy for smooth wire sending and constant tension in multiwire slicer[J]. IEEE Transactions on Industrial Informatics,2019,15(3): 1668-1677. doi: 10.1109/TII.2018.2878709 [13] MITSANTISUK C,OHISHI K,KATSURA S. Control of interaction force of twin direct-drive motor system using variable wire rope tension with multisensor integration[J]. IEEE Transactions on Industrial Electronics,2012,59(1): 498-510. doi: 10.1109/TIE.2011.2130494 [14] GASSMANN V,KNITTEL D,PAGILLA P R,et al. Fixed-order H∞ tension control in the unwinding section of a web handling system using a pendulum dancer[J]. IEEE Transactions on Control Systems Technology,2012,20(1): 173-180. [15] 李鹏威. 先进控制理论在冷轧平整机控制系统中的应用研究[D]. 北京: 北京科技大学, 2019.LI Pengwei. Application research of advanced control theory in control system of cold rolling temper mill[D]. Beijing: University of Science and Technology Beijing, 2019. (in Chinese) [16] LEE J,LEE C. Model-based winding tension profile to minimize radial stress in a flexible substrate in a roll-to-roll web transporting system[J]. IEEE/ASME Transactions on Mechatronics,2018,23(6): 2928-2939. doi: 10.1109/TMECH.2018.2873244 [17] 郭吉丰,王班,谭春林,等. 空间非合作目标物柔性捕获技术进展[J]. 宇航学报,2020,41(2): 125-135.GUO Jifeng,WANG Ban,TAN Chunlin,et al. Development of flexible capture technology for space non-cooperative target[J]. Journal of Astronautics,2020,41(2): 125-135. (in Chinese) [18] 郭吉丰,易琳,王班,等. 空间绳网多收口质量块收口过程动力学分析[J]. 宇航学报,2017,38(7): 669-677.GUO Jifeng,YI Lin,WANG Ban,et al. Dynamic analysis of take-up process for space tethered-net[J]. Journal of Astronautics,2017,38(7): 669-677. (in Chinese) [19] MAZUMDAR A,SPENCER S J,HOBART C,et al. Synthetic fiber capstan drives for highly efficient, torque controlled, robotic applications[J]. IEEE Robotics and Automation Letters,2017,2(2): 554-561. doi: 10.1109/LRA.2016.2646259 [20] 蒋辉虎. 舰载机着舰阻拦规律研究[D]. 哈尔滨: 哈尔滨工程大学, 2019.JIANG Huihu. Research on the arresting law of carrier-based aircraft landing[D]. Harbin: Harbin Engineering University, 2019. (in Chinese) [21] 张晓谞,张育兴,刘勇,等. 阻拦索张力控制方法[J]. 国防科技大学学报,2016,38(6): 49-53.ZHANG Xiaoxu,ZHANG Yuxing,LIU Yong,et al. Method of arresting cable tension control[J]. Journal of National University of Defense Technology,2016,38(6): 49-53. (in Chinese) [22] 杨志达. 空间系绳用永磁电机张力伺服系统控制技术研究[D]. 南京: 南京航空航天大学, 2020.YANG Zhida. Research on control technology of permanent magnet motor tension servo system for space tether[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2020. (in Chinese) -

下载: