|
|
论文:2019,Vol:37,Issue(2):273-282 |
|
|
引用本文： |
|
|
刘翔, 梁晓庚. 攻击角约束多拦截弹协同制导控制一体化研究[J]. 西北工业大学学报 |
|
|
LIU Xiang, LIANG Xiaogeng. Integrated Guidance and Control of Multiple Interceptors with Impact Angle Constraints Considered[J]. Northwestern polytechnical university |
|
|
|
|
|
|
|
| 攻击角约束多拦截弹协同制导控制一体化研究 |
|
| 刘翔, 梁晓庚 |
|
| 西北工业大学 自动化学院, 陕西 西安 710072 |
| 摘要: |
| 针对带有攻击角约束的多拦截弹协同拦截问题，基于制导与控制一体化（IGC）方法，提出了一种带有攻击角约束的多拦截弹分布式协同控制算法。首先，基于弹目相对运动关系和拦截弹俯仰通道动力学方程，建立带有攻击角约束的拦截弹"领弹"IGC模型，利用变增益扩张状态观测器（TVGESO）对模型中的未知干扰进行估计，在此基础上，基于干扰估计值和非奇异动态面滑模控制设计"领弹"控制算法；其次，采用基于"领弹-从弹"的分布式网络模式，设计多拦截弹协同控制策略，可以得到拦截弹在俯仰通道2个方向的速度分量，利用运动学转换关系转化为速度和弹道倾角参考指令；最后，基于TVGESO和动态面滑模控制设计"从弹"的控制算法。仿真结果验证所设计的带有攻击角约束的多拦截弹协同IGC算法具有较好的稳定性。 |
| 关键词:
攻击角约束
制导控制一体化
扩张状态观测器
动态面滑模控制
分布式网络
协同控制策略
|
|
| Integrated Guidance and Control of Multiple Interceptors with Impact Angle Constraints Considered |
|
| LIU Xiang, LIANG Xiaogeng |
|
| School of Automation, Northwestern Polytechnical University, Xi'an 710072, China |
| Abstract: |
| To solve the multi-interceptor coordination problem and to intercept the target with impact angle constraint, a novel distributed cooperative control algorithm with impact angle constraint based on integrated guidance and control is proposed. First, the mathematic model of integrated guidance and control is established by combining the interceptor-target relative motion model with the dynamic equation of the interceptor on pitch plane. The time varying gain extended state observer is developed to estimate and compensate the unknown disturbance. Based on the estimated value and fast nonsingular dynamic surface sliding control method, the IGC algorithm of leader is given; Then, based on distributed cooperative "leader-follower" model, the cooperative control strategy of multi-interceptor is designed, and gives out speeds in two directions on pitch plane, which are transformed to the command of total velocity and trajectory angle based on kinematic relations. Finally, to control the follower, the time varying gain extended state observer and the dynamic surface sliding control method are adopted. The simulation results demonstrate the effectiveness of the distributed cooperative control algorithm. |
| Key words:
impact angle constraints
integrated guidance and control
extended state observer
dynamic surface sliding control
distributed cooperative control algorithm
cooperative control strategy
|
|
| 收稿日期: 2018-03-13
修回日期:
|
| DOI: 10.1051/jnwpu/20193720273 |
| 基金项目: 航空科学基金（2016ZC12005）资助 |
| 通讯作者:
Email： |
| 作者简介: 刘翔(1986-),西北工业大学博士研究生,主要从事飞行器制导与控制研究。
|
|
| 相关功能 |
|
|
|
|
| 作者相关文章 |
|
| 刘翔 在本刊中的所有文章 |
| 梁晓庚 在本刊中的所有文章 |
|
|
|
|
|
|
|
|
参考文献: |
|
|
[1] ZHAO S Y, ZHOU R, WEI C, et al. Design of Time-Constrained Guidance Laws via Virtual Leader Approach[J]. Chinese Journal of Aeronautics, 2010, 23(1):103-108
[2] 肖增博,雷虎民,滕江川,等. 多导弹协同制导规律研究现状及展望[J].航空兵器,2011(6):18-22 XIAO Zengbo, LEI Humin, TENG Jiangchuan, et al. The Present Status and Prospect of Multi-Missile Cooperative Guidance Law[J]. Aero Weaponry, 2011(6):18-22. (in Chinese)
[3] 薛文超,黄朝东,黄一. 飞行制导控制一体化设计方法综述[J].控制理论与应用,2013,30(12):1511-1520 XUE Wenchao, HUANG Chaodong, HUANG Yi. Design Methods for the Integrated Guidance and Control System[J]. Control Theory & Applications,2013,30(12):1511-1520. (in Chinese)
[4] HOU M Z, LIANG X L, DUAN G Z. Adaptive Block Dynamic Surface Control for Integrated Missile Guidance and Autopilot[J]. Chinese Journal of Aeronautics, 2013, 26(3):741-750
[5] RAN M P, WANG Q, HOU D L, et al. Back Stepping Design of Missile Guidance and Control Based on Adaptive Fuzzy Sliding Mode Control[J]. Chinese Journal of Aeronautics, 2014, 27(3):634-642
[6] SHTESSEL Y B, SHKOLNIKOV I A, Levant A. Guidance and Control of Missile Interceptor Using Second-Order Sliding Modes[J]. IEEE Trans on Aerospace and Electronic Systems, 2009, 45(1):110-124
[7] 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
[8] WU P, YANG M. Integrated Guidance and Control Design for Missile with Terminal Impact Angle Constraint Based on Sliding Mode Control[J]. Journal of Systems Engineering and Electronics, 2010, 21(4):623-628
[9] 董飞垚,雷虎民,周池军,等. 导弹鲁棒高阶滑模制导控制一体化研究[J].航空学报,2013,34(9):2212-2218 DONG Feiyao, LEI Humin, ZHOU Chijun, et al. Research of Intergrated Robust High Order Sliding Mode Guidance and Control for Missiles[J]. Acta Aeronautica et Astronautica Sinica,2013,34(9):2212-2218(in Chinese)
[10] LIANG X L, HOU M Z, DUAN G R. Integrated Guidance and Control for Missile in the Presence of Input Saturation and Angular Constrains[C]//Proceedings of the 32nd Chinese Control Conference, Xi'an, China, 2013:1070-1075
[11] LIANG X L, HOU M Z, DUAN G R. Adaptive Dynamic Surface Control for Integrated Missile Guidance and Autopilot in the Presence of Input Saturation[J]. Journal of Aerospace Engineering, 2015, 28(5):401-412
[12] 后德龙,陈彬,王青,等. 碰撞自规避多弹分布式协同制导与控制[J]. 控制理论与应用,2014,31(9):1133-1142 HOU Delong, CHEN Bin, WANG Qing, et al. Collision Avoidance Multi-Missiles Distributed Cooperative Guidance and Control[J]. Control Theory and Applications, 2014, 31(9):1133-1142(in Chinese)
[13] 赵启伦,陈建,董希旺,等. 拦截高超声速目标的异类导弹协同制导律[J]. 航空学报, 2016, 37(3):936-948 ZHAO Qilun, CHEN Jian, DONG Xiwang et al. Cooperative Guidance Law for Heterogeneous Missiles Intercepting Hypersonic Weapon[J]. Acta Aeronautica et Astronautica Sinica, 2016,37(3):936-948(in Chinese)
[14] 周慧波,宋申民,郑重. 导弹编队协同攻击分布式鲁棒自适应控制[J].中国惯性技术学报,2015, 23(4):516-527 ZHOU Huibo, SONG Shenmin, ZHENG Zhong. Distributed Robust Adaptive Control for Missile Cooperative Engagement within Formation[J]. Journal of Chinese Inertial Technology, 2015, 23(4):516-527(in Chinese)
[15] 王晓芳,郑艺裕,林海. 导弹协同作战四维制导与控制一体化设计方法[J].系统工程与电子技术, 2015, 37(4):874-881 WANG Xiaofang, ZHENG Yiyu, LIN Hai. 4D Integrated Guidance and Control Law for Missiles Cooperative Engagement[J]. Systems Engineering and Electronics, 2015, 37(4):874-881(in Chinese)
[16] 张春研,宋建梅,候博,等. 带落角和时间约束的网络化导弹协同制导律[J]. 兵工学报,2016, 37(3):431-438 ZHANG Chunyan, SONG Jianmei, HOU Bo, et al. Cooperative Guidance Law with Impact Angle and Impact Time Constraints for Networked Missiles[J]. Acta Armamentarii, 2016, 37(3):431-438(in Chinese)
[17] 宋俊红,宋申民,徐胜利. 带有攻击角约束的多导弹协同制导律[J]. 中国惯性技术学报, 2016, 24(4):554-560 SONG Junhong, SONG Shenmin, XU Shengli. Cooperative Guidance Law for Multiple Missiles with Impact Angle Constraints[J]. Journal of Chinese Inertial Technology, 2016, 24(4):554-560(in Chinese)
[18] 孙胜,张华明,周荻. 考虑自动驾驶仪动特性的终端角速约束滑模导引律[J]. 宇航学报, 2013, 34(1):69-78 SUN Sheng, ZHANG Huaming, ZHOU Di. Sliding Mode Guidance Law with Autopilot Lag for Terminal Angle Constrained Trajectories[J]. Journal of Astronautics, 2013, 34(1):69-78(in Chinese)
[19] 卢晓东,赵辉,赵斌,等. 基于干扰补偿的拦截弹制导控制一体化设计[J]. 控制与决策,2017,32(10):1782-1788 LU Xiaodong, ZHAO Hui, ZHAO Bin, et al. Disturbance Compensation-Based Integrated Guidance and Control Design for Near Space Interceptor[J]. Control and Decision, 2017, 32(10):1782-1788(in Chinese) |
|
|
|
|
|
|
|
