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2023 | OriginalPaper | Chapter

Research on Robust Adaptive Guidance Law Against Target Arbitrary Maneuvering

Authors : Zhang Peng, Lu Hao, Fu Shu Tang, Luo Xu Tao

Published in: Proceedings of the 10th Chinese Society of Aeronautics and Astronautics Youth Forum

Publisher: Springer Nature Singapore

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Abstract

The augmented proportional navigation guidance law(APNGL), which is widely used at present, has poor robustness and large miss distance when it against escape target with large overload at the end of the trajectory. In order to solve this problem, firstly, the planar guidance model is established, a new guidance error is defined. Secondly, based on the principle of parallel approach method, a sliding mode adaptive guidance law is designed. In this process, there is no need to assume a target motion model or maneuver style, so the new guidance law is robust to target maneuvering and is suitable for engineering application. Thirdly, the miss-distance-index (MDI) is defined to evaluate the miss distance, and the guidance parameters are adjusted adaptively according to MDI. Finally, digital simulation was done in planar and 6-DOF, simulation results show that the designed guidance law has excellent guidance performance and can greatly reduce the average miss distance (the maximum can be more than 60%).

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Literature
1.
go back to reference Fan, H., Zhang, P.: The challenges for air-to-air missile. Aero Weaponry 2, 3–7 (2017). (in Chinese) Fan, H., Zhang, P.: The challenges for air-to-air missile. Aero Weaponry 2, 3–7 (2017). (in Chinese)
2.
go back to reference Fan, H., Yan, J.: The important development direction of airborne missile: autonomization. Aero Weaponry 26(1), 1–10 (2019). (in Chinese) Fan, H., Yan, J.: The important development direction of airborne missile: autonomization. Aero Weaponry 26(1), 1–10 (2019). (in Chinese)
3.
go back to reference Zarchan, P.: Tactical and Strategic Missile Guidance. 6th edn. American Institute of Aeronautics and Astronautics, Inc., (2012) Zarchan, P.: Tactical and Strategic Missile Guidance. 6th edn. American Institute of Aeronautics and Astronautics, Inc., (2012)
4.
go back to reference Stallard, D.V.: Discrete optimal terminal guidance for maneuvering target. J. Spacecr. Rockets 1, 381–382 (1977) Stallard, D.V.: Discrete optimal terminal guidance for maneuvering target. J. Spacecr. Rockets 1, 381–382 (1977)
5.
go back to reference Asher, R.B., Matuzeusk, J.H.: Optimal guidance for maneuvering targets. J. Spacecr. Rockets 6, 204–206 (1974) Asher, R.B., Matuzeusk, J.H.: Optimal guidance for maneuvering targets. J. Spacecr. Rockets 6, 204–206 (1974)
6.
go back to reference Li, F., Jia, S., Bu, K., et al.: Maneuvering and guidance dynamics compensated for guidance law. J. Ordnance Equipment Eng. 39(12), 20-24 (2018). (in Chinese) Li, F., Jia, S., Bu, K., et al.: Maneuvering and guidance dynamics compensated for guidance law. J. Ordnance Equipment Eng. 39(12), 20-24 (2018). (in Chinese)
7.
go back to reference Oshman, Y., Rad, D.A.: Differential-game based guidance law using target orientation observations. IEEE Trans. Aerosp. Electron. Syst. 42(1), 316–326 (2006) Oshman, Y., Rad, D.A.: Differential-game based guidance law using target orientation observations. IEEE Trans. Aerosp. Electron. Syst. 42(1), 316–326 (2006)
8.
go back to reference Zhang, Q.: Study of high-maneuvering target tracking and differential game guidance law design. Harbin Engineering University, pp. 30–44 (2017). (in Chinese) Zhang, Q.: Study of high-maneuvering target tracking and differential game guidance law design. Harbin Engineering University, pp. 30–44 (2017). (in Chinese)
9.
go back to reference Guo, Z., Zhou, S., Yu, Y.: Research of cooperative norm differential games guidance law for intercepting a maneuvering target. Comput. Simul. 37(3), 23-26 (2020). (in Chinese) Guo, Z., Zhou, S., Yu, Y.: Research of cooperative norm differential games guidance law for intercepting a maneuvering target. Comput. Simul. 37(3), 23-26 (2020). (in Chinese)
10.
go back to reference Zhang, S., Liu, X., Li, B., et al.: Study on maneuver penetration guidance law of ballistic missile based on differential games in the terminal of interception. Missiles Space Vehic. 2, 81–84 (2015). (in Chinese) Zhang, S., Liu, X., Li, B., et al.: Study on maneuver penetration guidance law of ballistic missile based on differential games in the terminal of interception. Missiles Space Vehic. 2, 81–84 (2015). (in Chinese)
11.
go back to reference Kang, S., Kim, H.J.: Differential game missile guidance with impact angle and time constraints, 3920–3925 (2011) Kang, S., Kim, H.J.: Differential game missile guidance with impact angle and time constraints, 3920–3925 (2011)
12.
go back to reference Anderson, G.M., Zong, Y.D.: Comparison of missile guidance law between optimal control interception and differential game interception. Syst. Eng. Electron. 5, 16–24 (1982) Anderson, G.M., Zong, Y.D.: Comparison of missile guidance law between optimal control interception and differential game interception. Syst. Eng. Electron. 5, 16–24 (1982)
13.
go back to reference Yuan, Y.: Nonlinear guidance law for interception of maneuvering target. Harbin Institute of Technology, pp. 81–100 (2008). (in Chinese) Yuan, Y.: Nonlinear guidance law for interception of maneuvering target. Harbin Institute of Technology, pp. 81–100 (2008). (in Chinese)
14.
go back to reference Li, J., Chen, J., Hu, H.: A nonlinear terminal guidance law for maneuver targets. J. Astronaut. 19(2), 37–42 (1998). (in Chinese) Li, J., Chen, J., Hu, H.: A nonlinear terminal guidance law for maneuver targets. J. Astronaut. 19(2), 37–42 (1998). (in Chinese)
15.
go back to reference Li, X., Xu, B., Li, S.: Feedback linearization with active disturbance rejection for entry guidance. In: Control Conference (CCC), 2019 38th Chinese. Nanjing University of Aeronautics and Astronautics, pp. 4202–4207 (2019) Li, X., Xu, B., Li, S.: Feedback linearization with active disturbance rejection for entry guidance. In: Control Conference (CCC), 2019 38th Chinese. Nanjing University of Aeronautics and Astronautics, pp. 4202–4207 (2019)
16.
go back to reference Cardona, S., Ospina, S., Giraldo, E.: Sliding mode control based on feedback linearization for a ball and beam system. In: 2019 IEEE 4th Colombian Conference on Automatic Control (CCAC), October 15–18 (2019) Cardona, S., Ospina, S., Giraldo, E.: Sliding mode control based on feedback linearization for a ball and beam system. In: 2019 IEEE 4th Colombian Conference on Automatic Control (CCAC), October 15–18 (2019)
17.
go back to reference Zhang, X., Liu, M., Li, Y., et al.: Impact angle control over composite guidance law based on feedback linearization and finite time control. J. Syst. Eng. Electron. 29(5), 1036– 1045 (2018) Zhang, X., Liu, M., Li, Y., et al.: Impact angle control over composite guidance law based on feedback linearization and finite time control. J. Syst. Eng. Electron. 29(5), 1036– 1045 (2018)
18.
go back to reference Shtessel, Y.B., Shkolnikov, I.A., Levant, A.: Guidance and control of missile interceptor using second-order sliding modes. IEEE Trans. Aerosp. Electron. Syst. 45(1), 110–124 (2009)CrossRef Shtessel, Y.B., Shkolnikov, I.A., Levant, A.: Guidance and control of missile interceptor using second-order sliding modes. IEEE Trans. Aerosp. Electron. Syst. 45(1), 110–124 (2009)CrossRef
19.
go back to reference Harl, N., Balakrishnan, S.N.: Impact time and angle guidance with sliding mode control. IEEE Trans. Control Syst. Technol. 20(6), 1436–1449 (2012)CrossRef Harl, N., Balakrishnan, S.N.: Impact time and angle guidance with sliding mode control. IEEE Trans. Control Syst. Technol. 20(6), 1436–1449 (2012)CrossRef
20.
go back to reference Zhang, W., Fu, S., Li, W., et al.: An impact angle constraint integral sliding mode guidance law for maneuvering targets interception. J. Syst. Eng. Electron. 31(1), 168–184 (2020) Zhang, W., Fu, S., Li, W., et al.: An impact angle constraint integral sliding mode guidance law for maneuvering targets interception. J. Syst. Eng. Electron. 31(1), 168–184 (2020)
21.
go back to reference Hu, Q., Han, T.: Sliding-mode impact time guidance law design for various target motions. J. Guidance, Contr. Dyn. 42(1), 136–148 (2019) Hu, Q., Han, T.: Sliding-mode impact time guidance law design for various target motions. J. Guidance, Contr. Dyn. 42(1), 136–148 (2019)
22.
go back to reference He, C., Shi, Z., Zheng, Y., et al.: Adaptive sliding mode cooperative guidance law against maneuvering target. In: Proceedings of the 37th Chinese Control Conference July 25–27, 2018, Wuhan, China He, C., Shi, Z., Zheng, Y., et al.: Adaptive sliding mode cooperative guidance law against maneuvering target. In: Proceedings of the 37th Chinese Control Conference July 25–27, 2018, Wuhan, China
23.
go back to reference Wei, X., Yang, J.: Time-varying terminal sliding mode based on salvo attack cooperative guidance law for unknown uncertainty upper bounds. In: Proceedings of the 35th Chinese Control Conference July 27–29, 2016, Chengdu, China Wei, X., Yang, J.: Time-varying terminal sliding mode based on salvo attack cooperative guidance law for unknown uncertainty upper bounds. In: Proceedings of the 35th Chinese Control Conference July 27–29, 2016, Chengdu, China
24.
go back to reference Becan, M.R.: Fuzzy guidance in the aerodynamic homing missiles. In: Preceedings of International Conference on Computational Intelligence, pp. 266–269 (2004) Becan, M.R.: Fuzzy guidance in the aerodynamic homing missiles. In: Preceedings of International Conference on Computational Intelligence, pp. 266–269 (2004)
25.
go back to reference Rajasekhar, V.: Fuzzy logic implementation of proportional navigation guidance. Acta Astronacitica 46(1), 17–24 (2000)MathSciNetCrossRef Rajasekhar, V.: Fuzzy logic implementation of proportional navigation guidance. Acta Astronacitica 46(1), 17–24 (2000)MathSciNetCrossRef
26.
go back to reference Suiyang, K., Zhihong, M., Shenkui, Z.: Adaptive fuzzy multi-surface sliding mode control for a class of nonlinear systems. In: 2007 Second IEEE Conference on Industrial Electronics and Applications, pp. 1095–1100 Suiyang, K., Zhihong, M., Shenkui, Z.: Adaptive fuzzy multi-surface sliding mode control for a class of nonlinear systems. In: 2007 Second IEEE Conference on Industrial Electronics and Applications, pp. 1095–1100
27.
go back to reference Xu, B., Li, X., Li, S., et al.: Intelligent guidance method based on nonlinear model predictive control for Mars atmospheric entry. Syst. Eng. Electron. 43(7), 1943–1953 (2021). (in Chinese) Xu, B., Li, X., Li, S., et al.: Intelligent guidance method based on nonlinear model predictive control for Mars atmospheric entry. Syst. Eng. Electron. 43(7), 1943–1953 (2021). (in Chinese)
28.
go back to reference Fang, Y., Deng, T., Fu, W.: An overview on the intelligent guidance law. Unmanned Syst. Technol. 3(6), 36-42 (2020). (in Chinese) Fang, Y., Deng, T., Fu, W.: An overview on the intelligent guidance law. Unmanned Syst. Technol. 3(6), 36-42 (2020). (in Chinese)
29.
go back to reference Li, S.,Yang, B., et al.: Space craft guidance and control based on artificial intelligence: review. Acta Aeronautica et Astronautica Sinica 42(4), 524201 (2021). (in Chinese) Li, S.,Yang, B., et al.: Space craft guidance and control based on artificial intelligence: review. Acta Aeronautica et Astronautica Sinica 42(4), 524201 (2021). (in Chinese)
Metadata
Title
Research on Robust Adaptive Guidance Law Against Target Arbitrary Maneuvering
Authors
Zhang Peng
Lu Hao
Fu Shu Tang
Luo Xu Tao
Copyright Year
2023
Publisher
Springer Nature Singapore
DOI
https://doi.org/10.1007/978-981-19-7652-0_17

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