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论文:2022,Vol:40,Issue(5):1109-1115 |
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引用本文： |
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齐照辉, 张今, 王远卓, 王嘉, 徐梦荣, 张程. 基于自适应超螺旋滑模弹道跟踪控制方法[J]. 西北工业大学学报 |
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QI Zhaohui, ZHANG Jin, WANG Yuanzhuo, WANG Jia, XU Mengrong, ZHANG Cheng. Trajectory tracking control method based on adaptive super-twisting sliding mode[J]. Journal of Northwestern Polytechnical University |
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| 基于自适应超螺旋滑模弹道跟踪控制方法 |
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| 齐照辉1, 张今2, 王远卓2,3, 王嘉1, 徐梦荣1, 张程4 |
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1. 航天飞行器生存技术与效能评估实验室, 北京 100089;
2. 西北工业大学 航天学院, 陕西 西安 710072;
3. 北京航空航天大学 宇航学院, 北京 100191;
4. 西安邮电大学 自动化学院, 陕西 西安 710121 |
| 摘要: |
| 针对导弹组网编队飞行过程中弹道跟踪控制问题,求解两点边值问题得到最优标称轨迹,结合滑模控制器抗干扰特性,提出了基于自适应超螺旋滑模弹道跟踪控制器设计方法。在末制导模型的基础上通过非线性规划的思想求解两点边值问题进而得到最优标称轨迹;结合自适应超螺旋滑模算法设计了基于状态偏差的跟踪控制器;引入LQR弹道跟踪控制法作为对比方法,通过仿真验证了在存在初始状态误差下滑模弹道跟踪方法的有效性和可行性,并通过蒙特卡罗仿真验证了该方法在不同初始状态偏差下仍具有良好的轨迹跟踪控制效果。 |
| 关键词:
轨迹跟踪
自适应超螺旋滑模控制
蒙特卡罗
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| Trajectory tracking control method based on adaptive super-twisting sliding mode |
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| QI Zhaohui1, ZHANG Jin2, WANG Yuanzhuo2,3, WANG Jia1, XU Mengrong1, ZHANG Cheng4 |
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1. The Institute of Effectiveness Evaluation of Flying Vehicle, Beijing 100089, China;
2. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
3. School of Astronautics, Beihang University, Beijing 100191, China;
4. School of Automation, Xi'an University of Posts and Telecommunications, Xi'an 710121, China |
| Abstract: |
| Aiming at the problem of trajectory tracking control in the process of missile network formation flying, based on the optimal nominal trajectory obtained by solving the two-point boundary value problem, combined with the anti-jamming characteristics of the sliding mode controller, a trajectory tracking control method based on the adaptive super-twisting sliding mode is proposed. First, on the basis of the terminal guidance section model, the two-point boundary value problem is solved through the idea of nonlinear programming to obtain the optimal nominal trajectory; Secondly, the tracking controller based on state deviation is designed in combination with the adaptive super-twisting sliding mode algorithm; Finally, the LQR trajectory tracking control method is introduced as a comparison method, and the effectiveness and feasibility of the sliding mode trajectory tracking method in the presence of initial state errors are verified by simulations, and the Monte Carlo simulation shows that the proposed method has good trajectory tracking control effect in the presence of different initial state errors. |
| Key words:
trajectory tracking
adaptive super-twisting sliding mode control
Monte Carlo
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| 收稿日期: 2021-12-25
修回日期:
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| DOI: 10.1051/jnwpu/20224051109 |
| 基金项目: 航空科学基金(20180153002,20200001053001)资助 |
| 通讯作者: 王远卓(1999-),北京航空航天大学硕士研究生,主要从事飞行器制导与控制技术研究。e-mail:wangyuanzhuo@126.com
Email：wangyuanzhuo@126.com |
| 作者简介: 齐照辉(1977—),航天飞行器生存技术与效能评估实验室副研究员,主要从事导弹攻防仿真与效能评估研究。
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| 相关功能 |
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| 作者相关文章 |
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| 齐照辉 在本刊中的所有文章 |
| 张今 在本刊中的所有文章 |
| 王远卓 在本刊中的所有文章 |
| 王嘉 在本刊中的所有文章 |
| 徐梦荣 在本刊中的所有文章 |
| 张程 在本刊中的所有文章 |
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