Three-dimensional vector guidance law with impact time and angle constraints

被引:24
作者
Dong, Wei [1 ]
Wang, Chunyan [1 ]
Liu, Junhui [1 ]
Wang, Jianan [1 ]
Xin, Ming [2 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] Univ Missouri, Dept Mech & Aerosp Engn, Columbia, MO 65211 USA
基金
中国国家自然科学基金;
关键词
SLIDING-MODE GUIDANCE;
D O I
10.1016/j.jfranklin.2022.11.035
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The three-dimensional (3D) impact time and angle guidance problem is of great practical significance but remains open because of the coupling nonlinearity and multiple constraints. To solve this problem, a 3D vector guidance law is proposed in this paper to intercept a non-maneuvering target at the desired impact conditions. First, a 3D vector impact angle constrained guidance law with explicit time-to-go estimation is developed by extending the planar one into the 3D space. Then, the intercepting component of the above guidance law is augmented by a time-to-go feedback term, which leads to the proposed 3D vector impact time and angle guidance law. Stability analysis and parameter selection criteria are presented to show the advantageous features of the proposed design. In particular, the proposed guidance law does not require the switch logic, numerical algorithms, or decoupling strategy, which outperforms similar existing results in terms of continuous command and convenient implementation. Finally, several numerical simulations are performed to validate the theoretical findings. (c) 2022 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:693 / 718
页数:26
相关论文
共 50 条
[1]   Finite-Time Convergent Three-Dimensional Nonlinear Intercept Angle Guidance [J].
Biswas, Bhaskar ;
Maity, Arnab ;
Kumar, Shashi Ranjan .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2020, 43 (01) :146-153
[2]   Attitude tracking control for reentry vehicles using centralised robust model predictive control [J].
Chai, Runqi ;
Tsourdos, Antonios ;
Gao, Huijun ;
Chai, Senchun ;
Xia, Yuanqing .
AUTOMATICA, 2022, 145
[3]   Dual-Loop Tube-Based Robust Model Predictive Attitude Tracking Control for Spacecraft With System Constraints and Additive Disturbances [J].
Chai, Runqi ;
Tsourdos, Antonios ;
Gao, Huijun ;
Xia, Yuanqing ;
Chai, Senchun .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2022, 69 (04) :4022-4033
[4]   Design and Implementation of Deep Neural Network-Based Control for Automatic Parking Maneuver Process [J].
Chai, Runqi ;
Tsourdos, Antonios ;
Savvaris, Al ;
Chai, Senchun ;
Xia, Yuanqing ;
Chen, C. L. Philip .
IEEE TRANSACTIONS ON NEURAL NETWORKS AND LEARNING SYSTEMS, 2022, 33 (04) :1400-1413
[5]   Multiobjective Optimal Parking Maneuver Planning of Autonomous Wheeled Vehicles [J].
Chai, Runqi ;
Tsourdos, Antonios ;
Savvaris, Al ;
Chai, Senchun ;
Xia, Yuanqing ;
Chen, C. L. Philip .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2020, 67 (12) :10809-10821
[6]   Sliding-Mode Guidance for Simultaneous Control of Impact Time and Angle [J].
Chen, Xiaotian ;
Wang, Jinzhi .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2019, 42 (02) :394-401
[7]   Optimal control based guidance law to control both impact time and impact angle [J].
Chen, Xiaotian ;
Wang, Jinzhi .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 84 :454-463
[8]   A modified cooperative proportional navigation guidance law [J].
Chen, Yadong ;
Wang, Jianan ;
Wang, Chunyan ;
Shan, Jiayuan ;
Xin, Ming .
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2019, 356 (11) :5692-5705
[9]   Nonsingular Sliding Mode Guidance for Impact Time Control [J].
Cho, Dongsoo ;
Kim, H. Jin ;
Tahk, Min-Jea .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (01) :61-68
[10]   Modified Pure Proportional Navigation Guidance Law for Impact Time Control [J].
Cho, Namhoon ;
Kim, Youdan .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (04) :852-872