Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy
Terminal guidance law against the maneuvering target is always the focal point. Most of the literatures focus on estimating the acceleration of target and time to go in guidance law, which are difficult to acquire. This paper presents a terminal guidance law based on receding horizon control strateg...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Wiley
2017-01-01
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| Series: | Complexity |
| Online Access: | http://dx.doi.org/10.1155/2017/2750172 |
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| author | Zhenglong Wu Zhenyu Guan Chengwei Yang Jie Li |
| author_facet | Zhenglong Wu Zhenyu Guan Chengwei Yang Jie Li |
| author_sort | Zhenglong Wu |
| collection | DOAJ |
| description | Terminal guidance law against the maneuvering target is always the focal point. Most of the literatures focus on estimating the acceleration of target and time to go in guidance law, which are difficult to acquire. This paper presents a terminal guidance law based on receding horizon control strategy. The proposed guidance law adopts the basic framework of receding horizon control, and the guidance process is divided into several finite time horizons. Then, optimal control theory and target motion prediction model are used to derive guidance law for minimum time index function with continuous renewal of original conditions at the initial time of each horizon. Finally, guidance law performs repeated iteration until intercepting the target. The guidance law is of subprime optimal type, requiring less guidance information, and does not need to estimate the acceleration of target and time to go. Numerical simulation has verified that the proposed guidance law is more effective than traditional methods on constant and sinusoidal target with bounded acceleration. |
| format | Article |
| id | doaj-art-d0da84d0abb441b880a724c6c668880f |
| institution | Kabale University |
| issn | 1076-2787 1099-0526 |
| language | English |
| publishDate | 2017-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Complexity |
| spelling | doaj-art-d0da84d0abb441b880a724c6c668880f2025-02-03T06:12:54ZengWileyComplexity1076-27871099-05262017-01-01201710.1155/2017/27501722750172Terminal Guidance Law for UAV Based on Receding Horizon Control StrategyZhenglong Wu0Zhenyu Guan1Chengwei Yang2Jie Li3School of Mechatronical Engineering, Beijing Institute of Technology, No. 5, Zhongguancun South Street, Beijing 100081, ChinaBeijing Electro-Mechanical Engineering Institute, No. 40 Yungangbeili, Fengtai, Beijing 100074, ChinaSchool of Mechatronical Engineering, Beijing Institute of Technology, No. 5, Zhongguancun South Street, Beijing 100081, ChinaSchool of Mechatronical Engineering, Beijing Institute of Technology, No. 5, Zhongguancun South Street, Beijing 100081, ChinaTerminal guidance law against the maneuvering target is always the focal point. Most of the literatures focus on estimating the acceleration of target and time to go in guidance law, which are difficult to acquire. This paper presents a terminal guidance law based on receding horizon control strategy. The proposed guidance law adopts the basic framework of receding horizon control, and the guidance process is divided into several finite time horizons. Then, optimal control theory and target motion prediction model are used to derive guidance law for minimum time index function with continuous renewal of original conditions at the initial time of each horizon. Finally, guidance law performs repeated iteration until intercepting the target. The guidance law is of subprime optimal type, requiring less guidance information, and does not need to estimate the acceleration of target and time to go. Numerical simulation has verified that the proposed guidance law is more effective than traditional methods on constant and sinusoidal target with bounded acceleration.http://dx.doi.org/10.1155/2017/2750172 |
| spellingShingle | Zhenglong Wu Zhenyu Guan Chengwei Yang Jie Li Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy Complexity |
| title | Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy |
| title_full | Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy |
| title_fullStr | Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy |
| title_full_unstemmed | Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy |
| title_short | Terminal Guidance Law for UAV Based on Receding Horizon Control Strategy |
| title_sort | terminal guidance law for uav based on receding horizon control strategy |
| url | http://dx.doi.org/10.1155/2017/2750172 |
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