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International Journal of Automation and Computing 2018, Vol. 15 Issue (2) :218-227    DOI: 10.1007/s11633-016-0953-y
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Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints
Hui-Bo Zhou1,2, Jun-Hong Song2, Shen-Min Song2
1 School of Mathematical Sciences, Harbin Normal University, Harbin 150009, China;
2 Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China
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Abstract In order to improve the precision of guidance for the missile intercepting maneuvering targets, this paper proposes a sliding mode guidance law with impact angle constraints based on the equation of the relative motion of the missile and the target in a 2D plane. Two finite-time convergent guidance laws are proposed based on the nonsingular terminal sliding mode, while, two exponential convergent guidance laws involving dynamic delay are developed through applying the higher-order nonsingular terminal sliding mode. The simulations denote that, in all the four scenarios of the target s maneuvering, the guidance laws are able to inhibit the chattering phenomenon of the sliding modes effectively; and from an expected aspect angle, the missiles could attack the targets with high precision and fast speed.
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KeywordsAutopilot   impact angle   nonsingular terminal sliding mode   finite-time convergent   guidance     
Received: 2014-05-29; Revised: 2015-04-08; published: 2015-04-08
Fund:

This work was supported by National Natural Science Foundation of China (No. 61021002).

Corresponding Authors: Hui-Bo Zhou     Email: zhouhb0306@sina.com
About author: Hui-Bo Zhou received the B. Sc. degree in College of Mathematics and Systems Science from Shenyang Normal University in 2006. E-mail:zhouhb0306@sina.com;Jun-Hong Song received the B.S. degree in Applied Mathematics from Liaocheng University in 2010 and M.S. degree in Applied Mathematics from Harbin Institute of Technology in 2012. E-mail:songjunhong111@163.com;Shen-Min Song received the Ph.D. degree in Control Theory and Application from Harbin Institute of Technology in 1996. E-mail:songshenmin@hit.edu.cn
Cite this article:   
Hui-Bo Zhou, Jun-Hong Song, Shen-Min Song. Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints[J]. International Journal of Automation and Computing , vol. 15, no. 2, pp. 218-227, 2018.
URL:  
http://www.ijac.net/EN/10.1007/s11633-016-0953-y      或     http://www.ijac.net/EN/Y2018/V15/I2/218
 
[1] S Sun. Guidance laws with finite time convergence for homing missiles[D]. Harbin:Harbin Institute of Technology, 2010. (in Chinese)
[2] M Kim, K V Grider. Terminal guidance for impact attitude angle constrained flight trajectories[J]. IEEE Transactions on Aerospace and Electronic Systems, vol.9, no.5, pp. 852-859, 1973.
[3] H Chai, Z D Hu, Y Cao. A Survey of Guidance Law with Terminal Impact Angle Constraints[J]. Journal of Astronautics, vol.31, no.2, pp. 315-323, 2010.(in Chinese)
[4] A Ratnoo, D Ghose. Impact Angle Constrained Interception of Stationary Targets[J]. Journal of Guidance, Control, and Dynamics, vol.31,no.6, pp. 1816-1821,2008.
[5] T Shima. Intercept-angle guidance[J]. Journal of Guidance, Control, and Dynamics, vol.34, no.2, pp. 484-493, 2011.
[6] N Harl, S N Balakrishnan. Impact Time and Angle Guidance With Sliding Mode Control[J]. IEEE Trsnsactions on Control Systems Technology, vol.20, no.6, pp. 1436-1449, 2012.
[7] R K Shashi, R Sachit, G Debasish. Sliding-mode guidance and control for all-aspect interceptors with terminal angle constraints[J]. Journal of Guidance, Control, and Dynamics, vol.35, no.4, pp. 1230-1246, 2012.
[8] R Sachit, G Debasish. Terminal impact angle constrained guidance laws using variable structure systems theory[J]. IEEE Transactions on Control Systems Technology, vol.99, pp. 1-10, 2013.
[9] S Sun, H M Zhang, D Zhou. Sliding Mode Guidance Law with Autopilot Lag for Terminal Angle Constrained Trajectories[J]. Journal of Astronautics, vol.34, no.1, pp. 69-78, 2013. (in Chinese)
[10] W B Gao. Theory and design method for variable sliding mode control[M]. Beijing:Science Press, 1996. (in Chinese)
[11] H X Zhang, J S Fan, F Meng, et dl. A New double power reaching law for sliding mode control[J]. Control and Decision, vol.28, no.2, pp. 289-293, 2013. (in Chinese)
[12] S H Yu, X H Yu, B Y Shirinzadeh, et al. Continuous finite-time control for robotic manipulators with terminal sliding mode[J]. Automatica, vol.41, no.11, pp. 1957-1964, 2005.
[13] X H Yu, Z H Man. Fast terminal sliding-mode control design for nonlinear dynamical systems[J]. IEEE Transactions on Circuits and Systems I:Fundamental Theory and Applications,vol.49, no.2, pp. 261-264, 2002.
[14] M R Neila, D Tarak. Adaptive terminal sliding mode control for rigid robotic manipulators[J]. International Journal of Automation and Computing, vol.8, no.2, pp. 215-220,2011.
[15] Y Feng, X Yu, Z Man. Non-singular terminal sliding mode control of rigid manipulators[J]. Automatica, vol.38, no.12, pp. 2159-2167, 2002.
[16] S Sun, D Zhou. Three-Dimensional Nonlinear Guidance Law with Consideration of Autopilot Dynamics[J]. Journal of Astronautics, vol.34, no.1, pp. 69-78, 2005.(in Chinese)
[17] P Qu, D Zhou. Three-Dimensional Guidance Law Accounting for Second-order Dynamics of Missile Autopilot[J]. Acta Aeronautica et Astronautica Sinica, vol.32, no.25, pp. 2096-2105, 2011. (in Chinese)
[18] S Sun, D Zhou, W Hou. A guidance law with finite time convergence accounting for autopilot lag[J]. Aerospace Science and Technology, vol.25, no.1, pp. 132-137, 2013.
[19] K M Ma, F H He, Y Yao. Estimation of target maneuver acceleration and guidance law implementation in homing terminal guidance[J].Journal of Astronautics, vol.30, no.6, pp. 2213-2219, 2009.(in Chinese)
[20] Y G Hong, D Z Cheng. Analysis and Control of Nonlinear Systems[M]. Bei Jing:Press of Science. (in Chinese)
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