Three-dimensional cooperative guidance laws with impact velocity and impact angles constraints
In this paper, we propose a cooperative guidance algorithm designed to enable multiple missiles to simultaneously attack a target at desired terminal angles while maintaining control over their impact velocities. The three-dimensional (3-D) guidance laws incorporate a guidance law along the line-of-...
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| Vydáno v: | Aerospace science and technology Ročník 159; s. 109997 |
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| Médium: | Journal Article |
| Jazyk: | angličtina |
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Elsevier Masson SAS
01.04.2025
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| ISSN: | 1270-9638 |
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| Abstract | In this paper, we propose a cooperative guidance algorithm designed to enable multiple missiles to simultaneously attack a target at desired terminal angles while maintaining control over their impact velocities. The three-dimensional (3-D) guidance laws incorporate a guidance law along the line-of-sight (LOS) and additional guidance laws in the normal and lateral directions relative to the LOS. Initially, a nonlinear cooperative guidance law is developed along the LOS to achieve consensus in range-to-go for multiple missiles, ensuring that all missiles converge to a range-to-go of zero with the specified impact velocity. Additionally, by employing a fixed-time sliding manifold design with state index coefficients, the normal and lateral guidance laws ensure that the LOS angles converge to their desired values within a fixed time frame. The proposed guidance laws are robust, effectively suppressing system disturbances, such as unknown target acceleration treated as external disturbances. Finally, we validate the performance of the proposed guidance law in a 3-D guidance scenario through comprehensive simulation experiments.
•Proposes a 3-D cooperative guidance law with fixed-time convergence for dynamic battle conditions.•Introduces relative velocity constraints for missile stability and adjustable impact velocity.•Uses range-to-go for coordination, improving accuracy and performance. |
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| AbstractList | In this paper, we propose a cooperative guidance algorithm designed to enable multiple missiles to simultaneously attack a target at desired terminal angles while maintaining control over their impact velocities. The three-dimensional (3-D) guidance laws incorporate a guidance law along the line-of-sight (LOS) and additional guidance laws in the normal and lateral directions relative to the LOS. Initially, a nonlinear cooperative guidance law is developed along the LOS to achieve consensus in range-to-go for multiple missiles, ensuring that all missiles converge to a range-to-go of zero with the specified impact velocity. Additionally, by employing a fixed-time sliding manifold design with state index coefficients, the normal and lateral guidance laws ensure that the LOS angles converge to their desired values within a fixed time frame. The proposed guidance laws are robust, effectively suppressing system disturbances, such as unknown target acceleration treated as external disturbances. Finally, we validate the performance of the proposed guidance law in a 3-D guidance scenario through comprehensive simulation experiments.
•Proposes a 3-D cooperative guidance law with fixed-time convergence for dynamic battle conditions.•Introduces relative velocity constraints for missile stability and adjustable impact velocity.•Uses range-to-go for coordination, improving accuracy and performance. |
| ArticleNumber | 109997 |
| Author | Zhu, Mingjia Wang, Bo Fan, Huijin Li, Yajun Zhi, Yongran An, Binghe Liu, Lei |
| Author_xml | – sequence: 1 givenname: Yajun surname: Li fullname: Li, Yajun organization: National Key Laboratory of Science and Technology on Multispectral Information Processing, School of Artificial Intelligence and Automation, Huazhong University of Science and Technology, Wuhan 430074, China – sequence: 2 givenname: Mingjia surname: Zhu fullname: Zhu, Mingjia organization: Beijing Aerospace Technology Institute, Beijing, 10074, China – sequence: 3 givenname: Binghe surname: An fullname: An, Binghe organization: National Key Laboratory of Science and Technology on Multispectral Information Processing, School of Artificial Intelligence and Automation, Huazhong University of Science and Technology, Wuhan 430074, China – sequence: 4 givenname: Yongran orcidid: 0000-0003-4521-7900 surname: Zhi fullname: Zhi, Yongran organization: National Key Laboratory of Science and Technology on Multispectral Information Processing, School of Artificial Intelligence and Automation, Huazhong University of Science and Technology, Wuhan 430074, China – sequence: 5 givenname: Lei orcidid: 0000-0003-3606-122X surname: Liu fullname: Liu, Lei email: liulei@hust.edu.cn organization: National Key Laboratory of Science and Technology on Multispectral Information Processing, School of Artificial Intelligence and Automation, Huazhong University of Science and Technology, Wuhan 430074, China – sequence: 6 givenname: Huijin orcidid: 0000-0002-0370-173X surname: Fan fullname: Fan, Huijin organization: National Key Laboratory of Science and Technology on Multispectral Information Processing, School of Artificial Intelligence and Automation, Huazhong University of Science and Technology, Wuhan 430074, China – sequence: 7 givenname: Bo surname: Wang fullname: Wang, Bo organization: National Key Laboratory of Science and Technology on Multispectral Information Processing, School of Artificial Intelligence and Automation, Huazhong University of Science and Technology, Wuhan 430074, China |
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| Keywords | Impact velocity Fixed-time control Cooperative guidance algorithm Impact angle |
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| Title | Three-dimensional cooperative guidance laws with impact velocity and impact angles constraints |
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