考虑建模误差的拦截弹制导控制一体化设计

doi:10.3969/j.issn.1000-1093.2013.09.018

兵工学报 ›› 2013, Vol. 34 ›› Issue (9): 1167-1172.doi: 10.3969/j.issn.1000-1093.2013.09.018

考虑建模误差的拦截弹制导控制一体化设计

宋海涛^1,2, 张涛¹, 张国良², 杨伟锋^1,3

1. 清华大学自动化系, 北京100084; 2. 第二炮兵工程大学, 陕西西安710025; 3. 空军工程大学防空反导学院, 陕西西安710051

收稿日期:2013-04-23 修回日期:2013-04-23 上线日期:2013-11-11
作者简介:宋海涛(1983—),男,讲师,博士研究生。

Integrated Design of Interceptor Guidance and Control Considering Modeling Error

SONG Hai-tao^1,2, ZHANG Tao¹, ZHANG Guo-liang², YANG Wei-feng^1,3

1. Department of Automation, Tsinghua University, Beijing 100084, China; 2. The Second Artillery Engineering University, Xi'an 710025, Shaanxi, China; 3. Institute of Air and Defense, Air Force Engineering University, Xi'an 710051, Shaanxi, China

Received:2013-04-23 Revised:2013-04-23 Online:2013-11-11

摘要/Abstract

摘要：

针对拦截弹末段的制导控制问题,改善已有建模结果,采用智能控制方法设计一体化控制律。考虑近似线性化和忽略耦合因素引起的建模误差,采用模型误差补偿改进拦截弹动力学模型;结合弹目相对运动非线性模型,建立面向拦截弹末段的制导控制一体化(IGC)模型。对此非匹配型非线性系统,利用自适应动态面控制方法进行控制器设计,不仅消除系统非匹配不确定性对系统性能的影响,同时避免了传统反演法的微分膨胀问题,得到控制目标与执行机构指令之间的直接关系。通过与忽略建模误差的IGC 拦截仿真比较,实验结果表明本文IGC 控制效果的优越性。

关键词: 飞行器控制、导航技术, 拦截弹, 制导控制一体化, 建模误差, 自适应动态面控制

Abstract:

An integrated control law is designed by modifying the existing modeling results and using the intelligent control method for the guidance and control of interceptor during the terminal course. While the modeling error caused by approximate linearization and ignoring couplings is taken into consideration, a model error compensation is used to modify the interceptor dynamics. A nonlinear model for the integrated guidance and control (IGC) is obtained. The adaptive dynamic surface control is proposed for the controller design of this mismatched nonlinear system. The influence of mismatched uncertainties on the system performance is eliminated, and the term explosion in traditional backstepping method is voided. The integrated control law is used to establish a direct relationship between control objective and actuators command. Compared with the controller which ignores the modeling error in interception simulation, the proposed controller shows better interception performance.

Key words: control and navigation technology of aerocraft, interceptor, integrated guidance and control, modeling error, adaptive dynamic surface control

中图分类号:

TJ765

宋海涛, 张涛, 张国良, 杨伟锋. 考虑建模误差的拦截弹制导控制一体化设计[J]. 兵工学报, 2013, 34(9): 1167-1172.

SONG Hai-tao, ZHANG Tao, ZHANG Guo-liang, YANG Wei-feng. Integrated Design of Interceptor Guidance and Control Considering Modeling Error[J]. Acta Armamentarii, 2013, 34(9): 1167-1172.

参考文献

[1] Shima T, Idan M, Golan O M. Sliding-mode control for integrated missile autopilot guidance [J]. Journal of Guidance, Control, and Dynamics, 2006, 29(2): 250 -260. [2] Williams D E, Richman J, Friedland B. Design of an integrated strapdown guidance and control system for a tactical missile [C]//AIAA Guidance and Control Conference. Gatlinburg: AIAA,1983: 57 -66. [3] Williams D E, Friedland B, Richman J. Integrated guidance and control for combined command/ homing guidance [C] //Proceedings of the American Control Conference. Atlanta: IEEE, 1988:549 -554. [4] Shtessel Y B, Tournes C H. Integrated higher-order sliding mode guidance and autopilot for dual-control missiles [J]. Journal of Guidance, Control, and Dynamics, 2009, 32(1): 79 -94. [5] Shtessel Y B, Shkolnikov I A, Levant A. Guidance and control of missile interceptor using second-order sliding modes [J]. IEEE Transactions on Aerospace and Electronic Systems, 2009, 45(1):110 -124. [6] Foreman D C, Tournes C H, Shtessel Y B. Integrated missile flight control using quaternions and third-order sliding mode control [C] //Proceedings of the American Control Conference. Baltimore: IEEE, 2010: 1332 -1337. [7] Menon P K, Sweriduk G D, Ohlmeyer E J, et al. Integrated guidance and control of moving-mass actuated kinetic warheads [J].Journal of Guidance, Control, and Dynamics, 2004, 27(1): 118-126. [8] Vaddi S S, Menon P K, Ohlmeyer E J. Numerical state-dependent riccati equation approach for missile integrated guidance control [J]. Journal of Guidance, Control, and Dynamics, 2009, 32(2): 699 -703. [9] 顾文锦, 张汝川, 于进勇. 反舰导弹航向平面模糊滑模控制导引一体化研究[C] //中国控制与决策学术年会. 无锡:IEEE, 2007: 81 -84. GU Wen-jin, ZHANG Ru-chuan, YU Jin-yong. Research on fuzzy sliding mode control to integrated guidance/ autopilot for antiship missiles [C]//Proceedings of Chinese Control and Decision Conference. Wuxi: IEEE, 2007: 81 -84. (in Chinese) [10] HOU Ming-zhe, DUAN Guang-ren. Adaptive dynamic surface control for integrated missile guidance and autopilot [J]. International Journal of Automation & Computing, 2011, 8(1): 122 -127. [11] HOU Ming-zhe, DUAN Guang-ren. Integrated guidance and control of homing missiles against ground fixed targets [J]. Chinese Journal of Aeronautics, 2008, 21(2): 162 -168. [12] 段广仁, 侯明哲, 谭峰. 基于滑模方法的自适应一体化导引与控制律设计[J]. 兵工学报, 2010, 31(2): 191 -198. DUAN Guang-ren, HOU Ming-zhe, TAN Feng. Adaptive, integrated guidance and control law design using sliding-mode approach[J]. Acta Armamentarii, 2010, 31(2): 191 - 198. (in Chinese) [13] Swaroop D, Gerdes J C, Yip P P, et al. Dynamic surface control of nonlinear systems [C]//Proceedings of the American Control Conference. Albuquerque: IEEE, 1997: 3028 -3034. [14] ZHANG Tian-ping, ZHU Qing, YANG Yue-quan. Adaptive neural control of non-affine pure-feedback non-linear systems with input nonlinearity and perturbed uncertainties [J]. International Journal of Systems Science, 2012, 43(4): 691 -706.

[1]	李万礼，李炯，李明杰. 拦截弹中制导弹道在线快速规划方法[J]. 兵工学报, 2021, 42(12): 2617-2625.
[2]	周觐，雷虎民. 考虑零控拦截的中制导最优弹道修正[J]. 兵工学报, 2018, 39(8): 1515-1525.
[3]	张民，陈亮，陈欣. 基于简便约束粒子群优化算法的空空导弹μ-PID控制器设计[J]. 兵工学报, 2017, 38(1): 89-96.
[4]	胡东方，姬源浩. 基于灰关联决策的模块化光电吊舱可靠性分析[J]. 兵工学报, 2016, 37(8): 1506-1516.
[5]	张松, 侯明善. 飞行器轨迹优化的造型降维方法[J]. 兵工学报, 2016, 37(6): 1125-1130.
[6]	李强，卢宝刚，王晓辉，王永海，庄凌. 一种导弹终端侵彻多约束最优制导方法[J]. 兵工学报, 2016, 37(6): 1131-1137.
[7]	张翼飞，董受全，毕开波. 基于Hough变换和聚类的舰艇编队队形识别算法[J]. 兵工学报, 2016, 37(4): 648-655.
[8]	王红辉，杨绍卿，吴成富，郝峰，车晓涛. 旋转矢量在高动态全姿态飞行器运动方程中的应用[J]. 兵工学报, 2016, 37(3): 439-446.
[9]	张尧，郭杰，唐胜景，商巍，张浩强. 机动目标拦截含攻击角约束的新型滑模制导律[J]. 兵工学报, 2015, 36(8): 1443-1457.
[10]	李成，李建勋，童中翔，贾林通，张志波. 红外成像制导末端局部图像识别跟踪研究[J]. 兵工学报, 2015, 36(7): 1213-1221.
[11]	赵江，周锐. 基于倾侧角反馈控制的预测校正再入制导方法[J]. 兵工学报, 2015, 36(5): 823-830.
[12]	范世鹏，林德福，姚怀瑾，路宇龙，祁载康. 基于最优二次型理论的滚转导弹三回路驾驶仪设计与研究[J]. 兵工学报, 2015, 36(5): 831-838.
[13]	鲁天宇，尹健，杜肖，夏群利. 虚位技术对相控阵雷达导引头制导性能的影响[J]. 兵工学报, 2015, 36(12): 2262-2268.
[14]	王昭磊，王青，冉茂鹏，董朝阳. 基于自适应模糊滑模的复合控制导弹制导控制一体化反演设计[J]. 兵工学报, 2015, 36(1): 78-86.
[15]	汪民乐, 李勇. 诱饵掩护下的弹道导弹突防效能评估建模研究[J]. 兵工学报, 2014, 35(8): 1318-1323.

考虑建模误差的拦截弹制导控制一体化设计

Integrated Design of Interceptor Guidance and Control Considering Modeling Error

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