Volume 47 Issue 6
Jul.  2018
Turn off MathJax
Article Contents

Shi Zhen, He Chendi, Zheng Yan. Cooperative guidance law design with impact angle constraint based on second-order sliding mode controller[J]. Infrared and Laser Engineering, 2018, 47(6): 617006-0617006(8). doi: 10.3788/IRLA201847.0617006
Citation: Shi Zhen, He Chendi, Zheng Yan. Cooperative guidance law design with impact angle constraint based on second-order sliding mode controller[J]. Infrared and Laser Engineering, 2018, 47(6): 617006-0617006(8). doi: 10.3788/IRLA201847.0617006

Cooperative guidance law design with impact angle constraint based on second-order sliding mode controller

doi: 10.3788/IRLA201847.0617006
  • Received Date: 2018-01-05
  • Rev Recd Date: 2018-02-03
  • Publish Date: 2018-06-25
  • For the problem of multi-missiles intercepting single maneuvering target, the cooperative guidance law with impact time and angle constraints was presented. Firstly, considering the system dynamics equation and the multi-agent consensus algorithm, a second order sliding mode controller along the line of sight(LOS) was proposed based on integral sliding mode control concept to guarantee salvo interception. Then an higher order sliding mode observer (HOSMO) was designed to estimate external disturbances of the perpendicular to the LOS. In addition, the sliding mode controller with HOSMO was proposed to guarantee the LOS angles converge to desired commands and the LOS angle rates converge to zero. Moreover, the stability of the two subsystem channels were proved by Lyapunov theorem. Simulation results illustrate the effectiveness of the proposed cooperative guidance law.
  • [1] Wang Hui, Lin Defu, Qi Zaikang, et al. Time-varying optimal augmented proportional navigation and miss distance closed-form solutions[J]. Infrared and Laser Engineering, 2013, 42(3):692-698. (in Chinese)王辉, 林德福, 祁载康,等. 时变最优的增强型比例导引及其脱靶量解析研究[J]. 红外与激光工程, 2013, 42(3):692-698.
    [2] Zang Luyao, Hou Miao, Wang Hui, et al. A switched-gain proportional navigation applicable for infrared guidance munitions[J]. Infrared and Laser Engineering, 2017, 46(5):0504004. (in Chinese)臧路尧, 侯淼, 王辉,等. 一种适用于红外制导弹药的变增益比例导引律[J]. 红外与激光工程, 2017, 46(5):0504004.
    [3] Jeon I S, Lee J I, Tahk M J. Homing guidance law for cooperative attack of multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2015, 33(1):275-280.
    [4] Harl N, Balakrishnan S N. Impact time and angle guidance with sliding mode control[J]. IEEE Transactions on Control Systems Technology, 2012, 20(6):1436-1449.
    [5] Vitaly Shaferman, Tal Shima. Cooperative optimal guidance laws for imposing a relative intercept angle[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(8):1395-1408.
    [6] Zhao Shiyu, Zhou Rui. Multi-missile cooperative guidance using coordination variables[J]. Acta Aeronauticaet Astronautica Sinica, 2008, 29(6):1605-1611. (in Chinese)赵世钰, 周锐. 基于协调变量的多导弹协同制导[J]. 航空学报, 2008, 29(6):1605-1611.
    [7] Zhao J, Zhou R. Unified approach to cooperative guidance laws against stationary and maneuvering targets[J]. Nonlinear Dynamics, 2015, 81(4):1635-1647.
    [8] Zhang Youan, Ma Guoxin, Wang Xingping. Time-cooperative guidance for multi-missiles:a leader-follower strategy[J]. Acta Aeronauticaet Astronautica Sinica, 2009, 30(6):1109-1118. (in Chinese)张友安, 马国欣, 王兴平. 多导弹时间协同制导:一种领弹-被领弹策略[J]. 航空学报, 2009, 30(6):1109-1118.
    [9] Zhang Y, Ma G, Liu A. A distributed cooperative guidance aw for salvo attack of multiple anti-ship missiles[J]. Chinese Journal of Aeronautics, 2015, 28(5):1438-1450.
    [10] Zhang P, Hugh H T, Li X. Fault tolerance of cooperative interception using multiple flight vehicles[J]. Journal of the Franklin Institute, 2013, 350(9):2373-2395.
    [11] Song Junhong, Song Shenmin, Xu Shengli. A cooperative guidance law for multiple missiles to intercept maneuvering target[J]. Journal of Astronautics, 2016, 37(12):1432-1440. (in Chinese)宋俊红, 宋申民, 徐胜利. 一种拦截机动目标的多导弹协同制导律[J]. 宇航学报, 2016, 37(12):1432-1440.
    [12] Deng Yongting, Li Hongwen Wang Jianli, et al. Large telescope low speed control based on adaptive sliding mode control[J]. Chinese Optics, 2016, 9(6):713-720. (in Chinese)邓永停, 李洪文, 王建立,等. 基于自适应滑模控制的大型望远镜低速控制[J]. 中国光学, 2016, 9(6):713-720.
    [13] Taleb M, Plestan F. Adaptive robust controller based on integral sliding mode concept[J]. International Journal of Control, 2017, 89(9):1-23.
    [14] Zhao Changjun, Bai Yue, Gong Xun, et al. Hex-Rotor unmanned aerial vehicle controller and its flight experiment under aerodynamic disturbance[J]. Optics and Precision Engineering, 2015, 23(4):1088-1095. (in Chinese)赵常均, 白越, 宫勋,等. 气动干扰下的Hex-Rotor无人飞行器控制器及其飞行实验[J]. 光学精密工程, 2015, 23(4):1088-1095.
    [15] Liu Jing, Li Hongwen, Deng Yongting. Current adaptive sliding mode control based on disturbance observer for permanent magnet synchronous motor[J]. Optics and Precision Engineering, 2017, 25(5):1229-1241. (in Chinese)刘京, 李洪文, 邓永停. 基于扰动观测器的永磁同步电机电流环自适应滑模控制[J]. 光学精密工程, 2017, 25(5):1229-1241.
  • 加载中
通讯作者: 陈斌, bchen63@163.com
  • 1. 

    沈阳化工大学材料科学与工程学院 沈阳 110142

  1. 本站搜索
  2. 百度学术搜索
  3. 万方数据库搜索
  4. CNKI搜索

Article Metrics

Article views(479) PDF downloads(37) Cited by()

Related
Proportional views

Cooperative guidance law design with impact angle constraint based on second-order sliding mode controller

doi: 10.3788/IRLA201847.0617006
  • 1. College of Automation,Harbin Engineering University,Harbin 150001,China

Abstract: For the problem of multi-missiles intercepting single maneuvering target, the cooperative guidance law with impact time and angle constraints was presented. Firstly, considering the system dynamics equation and the multi-agent consensus algorithm, a second order sliding mode controller along the line of sight(LOS) was proposed based on integral sliding mode control concept to guarantee salvo interception. Then an higher order sliding mode observer (HOSMO) was designed to estimate external disturbances of the perpendicular to the LOS. In addition, the sliding mode controller with HOSMO was proposed to guarantee the LOS angles converge to desired commands and the LOS angle rates converge to zero. Moreover, the stability of the two subsystem channels were proved by Lyapunov theorem. Simulation results illustrate the effectiveness of the proposed cooperative guidance law.

Reference (15)

Catalog

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return