基于扰动观测器的导引头隔离度抑制方法研究

doi:10.3969/j.issn.1000-1093.2014.11.009

兵工学报 ›› 2014, Vol. 35 ›› Issue (11): 1790-1798.doi: 10.3969/j.issn.1000-1093.2014.11.009

基于扰动观测器的导引头隔离度抑制方法研究

徐娇¹，王江¹，宋韬¹，胡宽容²

(1.北京理工大学宇航学院，北京 100081； 2.西北工业集团有限公司，陕西西安 710043)

收稿日期:2013-11-26 修回日期:2013-11-26 上线日期:2015-01-05
作者简介:徐娇(1988—)女硕士研究生
基金资助:
国家自然科学基金项目（61172182）；北京理工大学基础研究基金项目（20130142017）；高动态导航技术北京市重点实验室开放课题项目（HDN201403）

A Disturbance Observer-based Inhibition Method for Disturbance Rejection Rate of Seeker

XU Jiao¹, WANG Jiang¹, SONG Tao¹， HU Kuan-rong²

(1.School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081，China;2.Northwest Industries Group Co., Ltd, Xi'an 710043, Shaanxi, China)

Received:2013-11-26 Revised:2013-11-26 Online:2015-01-05

摘要/Abstract

摘要： 干扰力矩引起的平台导引头隔离度不仅会影响导引头输出精度，还会增加导弹制导系统脱靶量。针对隔离度对导弹制导精度带来的严重问题，设计了基于扰动观测器（DOB）的隔离度在线抑制算法，并分别研究了导引头建模误差、探测器输出频率以及测量噪声对隔离度抑制效果的影响。研究结果表明：基于DOB的隔离度抑制算法能够有效实现对隔离度的在线抑制，但导引头建模误差、探测器输出频率以及测量噪声会一定程度降低隔离度的抑制效果。

关键词: 兵器科学与技术, 平台导引头隔离度, 干扰力矩, 脱靶量, 扰动观测器, 在线抑制

Abstract: The disturbance rejection rate (DRR) of seeker has the effect on the output accuracy of seeker and the guidance performance.An online inhibition method based on disturbance observer is proposed for the problems of the guidance precision of missile caused by DRR. The errors of seeker models, the output frequency of detector and the effect of measurement noise on DRR inhibition are presented. The result shows that the spring torque and the damping torque are the main factors of the DRR generation, and the missile guidance precision would be reduced. The online inhibition method based on disturbance observer can inhibit DRR effectively; but the errors of seeker models, the output frequency of the detector and the measurement noise reduce the inhibition effects to some extent.

Key words: ordnance science and technology, disturbance rejection rate, disturbance torque, miss distance, disturbance observer, online inhibition

中图分类号:

TJ765.3

徐娇，王江，宋韬，胡宽容. 基于扰动观测器的导引头隔离度抑制方法研究[J]. 兵工学报, 2014, 35(11): 1790-1798.

XU Jiao, WANG Jiang, SONG Tao， HU Kuan-rong. A Disturbance Observer-based Inhibition Method for Disturbance Rejection Rate of Seeker[J]. Acta Armamentarii, 2014, 35(11): 1790-1798.

参考文献

［1］ Zipfel P H . Modeling and simulation of aerospace vehicle dyna-mics[M]. Florida: American Institute of Aeronautics and Astronautics, 2000.
[2] Taylor J H, Price C F. Direct statistical analysis of missile gui-dance system via CADET[R]. Massachusetts: Analytic Sciences Corporation, 1976.
[3] Kwon Y S，Hwang H Y，Choi Y S. Stabilization loop design on direct drive gimbaled platform with low stiffness and heavy inertia[C]∥ International Conference on Control, Automation and Systems 2007. Seoul, Korea:IEEE,2007:320-325.
[4] 穆虹. 防空导弹雷达导引头设计[M]. 北京: 宇航出版社, 1996.
MU Hong. Design of air defense missile seeker[M]. Beijing: China Astronautic Publishing House, 1996.(in Chinese)
[5] Bhattacharya R N, Tao T V, Sadhu S. Control structures and properties of missile seekers[J]. Journal of the Institution of Engineers: Electrical Engineering Division, 2002, 82(3): 253-261.
[6] 朱华征，范大鹏，马东玺，等. 导引头伺服系统隔离度与测试[J]. 光学精密工程，2009, 17(8): 1993-1998.
ZHU Hua-zheng, FAN Da-peng, MA Dong-xi, et al. Disturbance isolation index of seeker servo system and its test[J]. Optics and Precision Engineering, 2009,17(8):1993-1998.(in Chinese)
[7] 李富贵, 夏群利, 崔晓曦，等. 导引头隔离度寄生回路对视线角速度提取的影响[J]. 宇航学报, 2013, 34(8): 1072-1077.
LI Fu-gui, XIA Qun-li, CUI Xiao-xi, et al. Effect of seeker disturbance rejection rate parasitic loop on line of sight rate extraction[J]. Journal of Astronautics, 2013,34(8): 1072-1077.(in Chinese)
[8] Kwon Y S，Hwang H Y，Choi Y S. Stabilization loop design on direct drive gim-baled platform with low stiffness and heavy inertia[C]∥ International Conference on Control, Automation and Systems.Seoul Korea:IEEE,2007.
[9] 杜运理，夏群利，祁载康. 导引头隔离度相位滞后对寄生回路稳定性影响研究[J]. 兵工学报，2011, 32(1): 28-32.
DU Yun-li, XIA Qun-li, QI Zai-kang. Research on effect of seeker disturbance rejection rate with phase lag on stability of parasitical loop[J]. Acta Armamentarii, 2011, 32 (1) : 28-32.(in Chinese)
[10] Masten M K. Applications of control theory to design of line-of-sight stabilization system[C]∥American Control Conference.Boston, MA:IEEE, 1985:1219-1222. .
[11] Lin C L,Hsiao Y H. Adaptive feedforward control for disturbance torque rejection in seeker stabilizing loop [J]. IEEE Transactions on Control Systems Technology, 2001, 9(1): 108-121.
[12] Chu Z Y，Sun F C，Cui J. Disturbance observer-based robust control of free-floating space manipulators[J]. IEEE Systems Journal, 2008, 2(1): 114-119.
[13] Chladny R R., Koch C R. Flatness-based tracking of an electromechanical variable valve timing actuator with disturbance observer feedforward compensation[J]. IEEE Transactions on Control System Technology, 2008, 16(4): 652-663.
[14] Yang Z J, Tsubakihara H, Kanae S, et al. A novel robust nonlinear motion controller with disturbance observer[J]. IEEE Transactions on Control Systems Technology, 2008, 16(1):137-147.
[15] Nesline F W, Zarchan P. Radome induced miss distance in aerodynamically controlled homing missiles,AIAA 84-1845[R]. Reston ,VA:AIAA, 1984.
[16] Dwivdi P N, Tiwari S N, Bhattacharya A. A ZEM based effective integrated estimation and guidance of interceptors in terminal phase[C]∥AIAA Conference on Guidance, Navigation ,and Control. Toronto, Ontario Canada:AIAA, 2010: 6669-6693.
[17] Zarchan P. Tactical and strategic missile guidance[M]. 5th ed. Virginia: American Institute of Aeronautics and Astronautics Inc, 2007.
[18] 蔡毅. 光电精确制导武器[M]. 北京：兵器工业出版社, 2013.
CAI Yi. Photoelectric precision guided weapon[M].Beijing: Publishing House of Ordnance Industry, 2013.(in Chinese)

[1]	苗双全，张宝泉，王明超，王新伟，沈宇. 基于扰动观测器的机载光电稳定平台自适应指数时变滑模控制[J]. 兵工学报, 2022, 43(7): 1636-1645.
[2]	周伯俊, 于传强，刘志浩，柯冰. 基于高压储能的特种车辆快速起竖技术与验证[J]. 兵工学报, 2022, 43(7): 1488-1497.
[3]	高月光，冯顺山，刘云辉，黄岐. 不同端盖厚度的圆柱形装药壳体破片初速分布[J]. 兵工学报, 2022, 43(7): 1527-1536.
[4]	王思卓，范世鹏，林德福，刘经纬. 考虑目标机动和落角约束的二阶滑模制导律[J]. 兵工学报, 2022, 43(12): 3048-3061.
[5]	崔梦曦，郝宏旭，王新星，孟亮飞，毛昱天，万轲，刘耘臻，张妍. 基于导引头-弹体耦合模型和伴随制导系统的火箭弹脱靶量快速估计方法[J]. 兵工学报, 2022, 43(10): 2554-2564.
[6]	何山，吴盘龙，李星秀，恽鹏，薄煜明. 基于刚体弹道模型的防空火控解算方法[J]. 兵工学报, 2020, 41(8): 1494-1501.
[7]	陈峰，何广军. 抗多径干扰的有限时间收敛制导律[J]. 兵工学报, 2018, 39(9): 1741-1748.
[8]	娄伟鹏，郑长松，李和言，陈建文，张周立，马源. 高速《Symbol》v湿式换挡离合器排油阀临界开启和关闭压力研究[J]. 兵工学报, 2017, 38(9): 1665-1672.
[9]	王宪成，杨绍卿，马宁，赵文柱. 车辆柴油机缸套动载荷磨损计算模型研究[J]. 兵工学报, 2017, 38(9): 1673-1680.
[10]	孙皓泽，常天庆，王全东，孔德鹏，戴文君. 一种基于分层多尺度卷积特征提取的坦克装甲目标图像检测方法[J]. 兵工学报, 2017, 38(9): 1681-1691.
[11]	张玉燕，孙莎莎，王振春，曹海要，战再吉. 高速载流电枢表面瞬态温度场仿真与测量[J]. 兵工学报, 2017, 38(9): 1692-1698.
[12]	李臣明，宦超，石怀龙. 某箱式火箭炮对面目标分布式杀伤最优火力分配[J]. 兵工学报, 2017, 38(9): 1699-1704.
[13]	雷娟棉，张嘉炜，谭朝明. 小攻角下船尾外形对旋转弹丸马格努斯效应影响的数值研究[J]. 兵工学报, 2017, 38(9): 1705-1715.
[14]	李泽，闫晓鹏，栗苹，郝新红，王建涛. 扫频式干扰对调频多普勒引信的干扰机理研究[J]. 兵工学报, 2017, 38(9): 1716-1722.
[15]	张浩为，谢军伟，张昭建，宗彬锋，陈唐军. 基于混合自适应遗传算法的相控阵雷达任务调度[J]. 兵工学报, 2017, 38(9): 1761-1770.

基于扰动观测器的导引头隔离度抑制方法研究

A Disturbance Observer-based Inhibition Method for Disturbance Rejection Rate of Seeker

PDF

可视化

被引次数

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价