Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations

Hang Guo; Qingfeng Yang; Zhiyuan Guo; Xiaofeng Zhang; Wenxing Fu; Jie Yan

doi:10.1007/978-981-99-0479-2_178

Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations

Hang Guo, Qingfeng Yang, Zhiyuan Guo, Xiaofeng Zhang, Wenxing Fu, Jie Yan

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

An impact time and angle cooperative guidance law was proposed for multiple missiles with coupled dynamics among velocity and normal accelerations to realize impact time and impact angle cooperation simultaneously. The coupling property was modeled concretely and introduced to the cooperative guidance design. With regarding to the impact time cooperation, flight velocity control was developed, while considering the coupling effects arising from normal accelerations in longitudinal and lateral plane. And besides, for the impact angle cooperation, an impact angle cooperative guidance (IACG) was derived on the basis of modified proportional navigation guidance (PNG), taking the velocity variation into account. In addition, the target was assumed to execute evasive maneuver. To depress the negative effects arising from the coupled dynamics among velocity and normal accelerations, the compensated parts in the velocity and normal accelerations control commands were designed on the concrete model of the coupled dynamics. Consequently, an ITACG was achieved to realize salvo attack with impact angle cooperation, and its effectiveness was verified by mathematical simulations.

Original language	English
Title of host publication	Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022
Editors	Wenxing Fu, Mancang Gu, Yifeng Niu
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	1916-1930
Number of pages	15
ISBN (Print)	9789819904785
DOIs	https://doi.org/10.1007/978-981-99-0479-2_178
State	Published - 2023
Event	International Conference on Autonomous Unmanned Systems, ICAUS 2022 - Xi'an, China Duration: 23 Sep 2022 → 25 Sep 2022

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	1010 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	International Conference on Autonomous Unmanned Systems, ICAUS 2022
Country/Territory	China
City	Xi'an
Period	23/09/22 → 25/09/22

Keywords

Coupled dynamics
Flight velocity control
Impact angle cooperative guidance (IACG)
Impact time and angle cooperative guidance (ITACG)

Access to Document

10.1007/978-981-99-0479-2_178

Cite this

Guo, H., Yang, Q., Guo, Z., Zhang, X., Fu, W., & Yan, J. (2023). Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations. In W. Fu, M. Gu, & Y. Niu (Eds.), Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022 (pp. 1916-1930). (Lecture Notes in Electrical Engineering; Vol. 1010 LNEE). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-99-0479-2_178

Guo, Hang ; Yang, Qingfeng ; Guo, Zhiyuan et al. / Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations. Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022. editor / Wenxing Fu ; Mancang Gu ; Yifeng Niu. Springer Science and Business Media Deutschland GmbH, 2023. pp. 1916-1930 (Lecture Notes in Electrical Engineering).

@inproceedings{44917dec4a8b47f89eec11b3c2cbe253,

title = "Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations",

abstract = "An impact time and angle cooperative guidance law was proposed for multiple missiles with coupled dynamics among velocity and normal accelerations to realize impact time and impact angle cooperation simultaneously. The coupling property was modeled concretely and introduced to the cooperative guidance design. With regarding to the impact time cooperation, flight velocity control was developed, while considering the coupling effects arising from normal accelerations in longitudinal and lateral plane. And besides, for the impact angle cooperation, an impact angle cooperative guidance (IACG) was derived on the basis of modified proportional navigation guidance (PNG), taking the velocity variation into account. In addition, the target was assumed to execute evasive maneuver. To depress the negative effects arising from the coupled dynamics among velocity and normal accelerations, the compensated parts in the velocity and normal accelerations control commands were designed on the concrete model of the coupled dynamics. Consequently, an ITACG was achieved to realize salvo attack with impact angle cooperation, and its effectiveness was verified by mathematical simulations.",

keywords = "Coupled dynamics, Flight velocity control, Impact angle cooperative guidance (IACG), Impact time and angle cooperative guidance (ITACG)",

author = "Hang Guo and Qingfeng Yang and Zhiyuan Guo and Xiaofeng Zhang and Wenxing Fu and Jie Yan",

note = "Publisher Copyright: {\textcopyright} 2023, Beijing HIWING Sci. and Tech. Info Inst.; International Conference on Autonomous Unmanned Systems, ICAUS 2022 ; Conference date: 23-09-2022 Through 25-09-2022",

year = "2023",

doi = "10.1007/978-981-99-0479-2_178",

language = "英语",

isbn = "9789819904785",

series = "Lecture Notes in Electrical Engineering",

publisher = "Springer Science and Business Media Deutschland GmbH",

pages = "1916--1930",

editor = "Wenxing Fu and Mancang Gu and Yifeng Niu",

booktitle = "Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022",

}

Guo, H, Yang, Q, Guo, Z, Zhang, X, Fu, W & Yan, J 2023, Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations. in W Fu, M Gu & Y Niu (eds), Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022. Lecture Notes in Electrical Engineering, vol. 1010 LNEE, Springer Science and Business Media Deutschland GmbH, pp. 1916-1930, International Conference on Autonomous Unmanned Systems, ICAUS 2022, Xi'an, China, 23/09/22. https://doi.org/10.1007/978-981-99-0479-2_178

Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations. / Guo, Hang; Yang, Qingfeng; Guo, Zhiyuan et al.
Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022. ed. / Wenxing Fu; Mancang Gu; Yifeng Niu. Springer Science and Business Media Deutschland GmbH, 2023. p. 1916-1930 (Lecture Notes in Electrical Engineering; Vol. 1010 LNEE).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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T1 - Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations

AU - Guo, Hang

AU - Yang, Qingfeng

AU - Guo, Zhiyuan

AU - Zhang, Xiaofeng

AU - Fu, Wenxing

AU - Yan, Jie

PY - 2023

Y1 - 2023

N2 - An impact time and angle cooperative guidance law was proposed for multiple missiles with coupled dynamics among velocity and normal accelerations to realize impact time and impact angle cooperation simultaneously. The coupling property was modeled concretely and introduced to the cooperative guidance design. With regarding to the impact time cooperation, flight velocity control was developed, while considering the coupling effects arising from normal accelerations in longitudinal and lateral plane. And besides, for the impact angle cooperation, an impact angle cooperative guidance (IACG) was derived on the basis of modified proportional navigation guidance (PNG), taking the velocity variation into account. In addition, the target was assumed to execute evasive maneuver. To depress the negative effects arising from the coupled dynamics among velocity and normal accelerations, the compensated parts in the velocity and normal accelerations control commands were designed on the concrete model of the coupled dynamics. Consequently, an ITACG was achieved to realize salvo attack with impact angle cooperation, and its effectiveness was verified by mathematical simulations.

AB - An impact time and angle cooperative guidance law was proposed for multiple missiles with coupled dynamics among velocity and normal accelerations to realize impact time and impact angle cooperation simultaneously. The coupling property was modeled concretely and introduced to the cooperative guidance design. With regarding to the impact time cooperation, flight velocity control was developed, while considering the coupling effects arising from normal accelerations in longitudinal and lateral plane. And besides, for the impact angle cooperation, an impact angle cooperative guidance (IACG) was derived on the basis of modified proportional navigation guidance (PNG), taking the velocity variation into account. In addition, the target was assumed to execute evasive maneuver. To depress the negative effects arising from the coupled dynamics among velocity and normal accelerations, the compensated parts in the velocity and normal accelerations control commands were designed on the concrete model of the coupled dynamics. Consequently, an ITACG was achieved to realize salvo attack with impact angle cooperation, and its effectiveness was verified by mathematical simulations.

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KW - Flight velocity control

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KW - Impact time and angle cooperative guidance (ITACG)

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Y2 - 23 September 2022 through 25 September 2022

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Guo H, Yang Q, Guo Z, Zhang X, Fu W , Yan J. Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations. In Fu W, Gu M, Niu Y, editors, Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022. Springer Science and Business Media Deutschland GmbH. 2023. p. 1916-1930. (Lecture Notes in Electrical Engineering). doi: 10.1007/978-981-99-0479-2_178

Impact Time and Angle Cooperative Guidance for Multiple Unmanned Air Vehicles (UAVs) with Coupled Dynamics Among Velocity and Normal Accelerations

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Keywords

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