Integral Global Sliding Mode Guidance for Impact Angle Control

Shaoming He; Defu Lin; Jiang Wang

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Integral Global Sliding Mode Guidance for Impact Angle Control

机译：整体全局滑模指导，用于冲击角控制

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摘要

This paper proposes a new guidance law based on integral sliding mode control (ISMC) technique for maneuvering target interception with impact angle constraint. A time-varying function weighted line-of-sight error dynamics, representing the nominal guidan

机译：提出了一种基于积分滑模控制（ISMC）技术的新的制导律，该制导律用于对具有冲击角约束的目标拦截进行机动。时变函数加权视线误差动态，表示名义guidan

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来源
《IEEE Transactions on Aerospace and Electronic Systems》 |2019年第4期|1843-1849|共7页
作者
Shaoming He; Defu Lin; Jiang Wang;
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作者单位

Cranfield University Cranfield U.K.;

Beijing Institute of Technology Beijing China;

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原文格式 PDF
正文语种 eng
中图分类
关键词
Aerodynamics; Convergence; Missiles; Closed-form solutions; Kinematics; Mathematical model;

机译：空气动力学收敛;导弹;封闭式解决方案;运动学数学模型;

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专利

1. An impact angle constraint integral sliding mode guidance law for maneuvering targets interception [J] . Systems Engineering and Electronics, Journal of . 2020,第1期

机译：机动目标拦截的冲击角约束积分滑模制导律
2. An impact angle constraint integral sliding mode guidance law for maneuvering targets interception [J] . ZHANG Wenjie, FU Shengnan, LI Wei, 系统工程与电子技术（英文版） . 2020,第001期

机译：机动目标拦截的冲击角约束积分滑模制导律
3. A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint [J] . Ming Chao, Wang Xiaoming, Sun Ruisheng Aerospace science and technology . 2019,第Nova期

机译：具有冲击角约束的新型非奇异终端滑模控制一体化导弹制导
4. Adaptive Integral Sliding Mode Guidance Law with Impact Angle Constraint Considering Autopilot Lag [C] . X B Li, G R Zhao, S Liu, International Conference on Artificial Intelligence, Automation and Control Technologies . 2020

机译：考虑自动驾驶率滞后的冲击角约束自适应积分滑动模式引导法
5. Missile Interceptor Integrated Guidance and Control: Single-Loop Higher-Order Sliding Mode Approach [D] . Cross, Michael. 2020

机译：导弹拦截器集成指导和控制：单环高阶滑动模式方法
6. Tensor Product Model Transformation Based Adaptive Integral-Sliding Mode Controller: Equivalent Control Method [O] . Guoliang Zhao, Kaibiao Sun, Hongxing Li 2013

机译：基于张量积模型变换的自适应积分滑模控制器：等效控制方法
7. Integral Global Sliding Mode Guidance for Impact Angle Control [O] . Shaoming He, Defu Lin, Jiang Wang 2019

机译：冲击角控制的整体全球滑模指导
8. Report from the Guidance and Control Panel Working Group 04 on the Impact of Global Positioning System on Guidance and Controls Systems Design of Military Aircraft. Volume I [R] . Howell, G. C. 1979

机译：指导和控制小组第04工作组关于全球定位系统对军用飞机制导和控制系统设计影响的报告。第一卷

Integral Global Sliding Mode Guidance for Impact Angle Control

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