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Research on Multi-missile Cooperative Guidance Law Based on Second-order Sliding Mode Control |
LIU Yue1, ZHANG Jialiang2, ZHAO Lijuan2, ZHEN Ziyang1 |
1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, Jiangsu, China;
2. Shanghai Electro-Mechanical Engineering Institute,Shanghai 201109, China |
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Abstract The paper proposes a cooperative guidance law with constraints on guidance time and attack angle in twodimension plane, which can improve the penetration ability and combat effectiveness of multi-missile systems and adapt to the complex and changeable future warfare. By applying the second-order sliding mode control theory and using the backstepping method to ensure the stability of the system, through setting the trajectory of the expected attack angle, the cooperative guidance law with multiple constraints is derived. The guidance law is simulated under the condition that the target is stationary or moving. The guidance law can complete the cooperative guidance task with time and angle constraints within a certain limit range of lateral acceleration.
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Received: 28 June 2020
Published: 30 September 2020
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LIU Xinyu, WANG Sen, ZENG Long, YUAN Shaoheng, HAO Zhenghang, LU Xinyan. An Adaptive Additional Control Strategy for Suppressing Low-Frequency Grid Oscillations in Doubly-Fed Wind Farms[J]. Journal of Shanghai Jiao Tong University, 2023, 57(9): 1156-1164. |
[2] |
LI Mengxuan, GUO Jianguo, XU Xinpeng, SHEN Yuheng. Guidance Law Based on Proximal Policy Optimization[J]. Air & Space Defense, 2023, 6(4): 51-57. |
[3] |
YUAN Dongdong (袁冬冬), WANG Yankai∗ (王彦恺). Data Driven Model-Free Adaptive Control Method for
Quadrotor Trajectory Tracking Based on
Improved Sliding Mode Algorithm[J]. J Shanghai Jiaotong Univ Sci, 2022, 27(6): 790-798. |
[4] |
GAO Bolun, LI Jian, LIU Ruiheng, LYU Shuo, ZHANG Xiaoyu, ZHANG Qingzhen. Research on Double Closed Loop Terminal Guidance Law with Terminal Angle Constraint[J]. Air & Space Defense, 2022, 5(4): 38-46. |
[5] |
LYU Shuo, ZHANG Qingzhen, GUO Yunhe, FENG Shuo. Attitude Control of Missile with Deflectable Nose Based on Backstepping Sliding Mode Control[J]. Air & Space Defense, 2022, 5(4): 30-37. |
[6] |
WANG Jiaqi, GUO Jianguo, GUO Zongyi, ZHAO Bin. Sliding Mode Control of High Mach Number Aircraft Based on Disturbance Observer[J]. Air & Space Defense, 2021, 4(3): 85-91. |
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ZHANG Xianku, HAN Xu. Modeling and Sliding Mode Control for Chaotic Yawing Phenomenon of Large Oil Tanker[J]. Journal of Shanghai Jiao Tong University, 2021, 55(1): 40-47. |
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[9] |
LIU Qiu, ZHAO Dongya. Discrete-Time Integral Sliding Mode Predictive Control for Single Input Single Output Systems[J]. Journal of Shanghai Jiaotong University, 2020, 54(9): 898-903. |
[10] |
ZHANG Xue, CUI Hao, LUO Qianyue, ZHANG Hui . Nonlinear Distributed Model Predictive Control for Multiple Missiles Against Maneuvering Target with a Trajectory Predictor[J]. J Shanghai Jiaotong Univ Sci, 2020, 25(6): 779-789. |
[11] |
CHANG Lu, SHAN Liang, LI Jun, DAI Yuewei . Sliding Mode Control of T-Shaped Pedestrian Channel[J]. Journal of Shanghai Jiao Tong University(Science), 2020, 25(4): 478-485. |
[12] |
ZHAO Bin, HUANG Xiaoyang, ZHOU Jun, GUO Yue. Multi-missile Distributed LOS Cooperative Guidance Law Design Based on Sliding Mode Control[J]. Air & Space Defense, 2020, 3(3): 16-23. |
[13] |
ZHANG Xiaoyu, ZHANG Peng, ZHENG Xin, NI Yuanhua. Terminal Angle Constraint Sliding Mode Guidance Law Design Based on Fixed-time Convergence[J]. Air & Space Defense, 2020, 3(3): 9-15. |
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YAO Laipeng, HOU Baolin, LIU Xi. Adaptive Terminal Sliding Mode Control of
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[15] |
ZHAO Bin, ZHU Chuanxiang, TONG Yun, HU Yang, JIANG Ruimin. Adaptive Sliding Mode Observer Based Impact Angle Constraint Guidance Law[J]. Air & Space Defense, 2019, 2(4): 19-24. |
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