Impact Time Control Guidance Law Considering Seeker's Field-of-View Constraint Without Time-to-Go Information

Zhe Yang; Defu Lin; Luyao Zang

doi:10.20965/jaciii.2016.p0412

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JACIII Vol.20 No.3 pp. 412-417

doi: 10.20965/jaciii.2016.p0412

(2016)

Paper:

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Impact Time Control Guidance Law Considering Seeker's Field-of-View Constraint Without Time-to-Go Information

Zhe Yang^†, Defu Lin, and Luyao Zang

School of Aerospace Engineering, Beijing Institute of Technology
Zhong Guan Cun South Street, Haidian District, Beijing 10081, China

^†Corresponding author

Received:

September 13, 2015

Accepted:

January 5, 2016

Published:

May 19, 2016

Keywords:

impact time control, field-of-view, time-to-go, sliding mode control, salvo attack

Abstract

Accurate time-to-go estimation with large heading angle error is difficult for homing guidance laws, especially for the impact time control. Considering this, a new cooperative guidance law which requires no time-to-go estimation is investigated. First, the impact time control problem is transformed to the look angle command tracking problem. The look angle command guarantees that the range-to-go error converges to zero asymptotically. Then the proposed guidance law considering the seeker's field-of-view constraint is derived using sliding mode control to track the desired look angle signal. Numerical simulations are performed to verify the effectiveness of the proposed guidance law for one-to-one and many-to-one engagement scenarios.

Cite this article as:

Z. Yang, D. Lin, and L. Zang, “Impact Time Control Guidance Law Considering Seeker's Field-of-View Constraint Without Time-to-Go Information,” J. Adv. Comput. Intell. Intell. Inform., Vol.20 No.3, pp. 412-417, 2016.

Data files:

References

[1] J. I. Lee, I. S. Jeon, and M. J. Tahk, “Guidance law to control impact time and angle,” IEEE Trans. on Aerospace and Electronic Systems, Vol.43, pp. 301-310, 2007.
[2] H. Nathan and S. N. Balakrishnan, “Impact Time and Angle Guidance with Sliding Mode Control,” IEEE Trans. on Control Systems Technology, Vol.20, pp. 1436-1449, 2012.
[3] Y. A. Zhang, G. X. Ma, and A. L. Liu, “Guidance law with impact time and impact angle constraints,” Chinese J. of Aeronautics, Vol.26, pp. 960-966, 2013.
[4] J. Zeng, L. Dou, and B. Xin, “Cooperative salvo attack using guidance law of multiple missiles,” J. of Advanced Computational Intelligence and Intelligent Informatics (JACIII), Vol.19, pp. 301-306, 2015.
[5] S. Kang and H. J. Kim, “Differential game missile guidance with impact angle and time constraints,” 18th IFAC World Congress, Milano, Italy, pp. 3920-3925, 2011.
[6] I. S. Jeon, J. I. Lee, and M. J. Tahk, “Impact-time-control guidance law for anti-ship missiles,” IEEE Trans. on Control Systems Technology, Vol.14, pp. 260-266, 2006.
[7] S. Zhao and R. Zhou, “Cooperative Guidance for Multimissile Salvo Attack,” Chinese J. of Aeronautics, Vol.21, pp. 533-539, 2008.
[8] S. R. Kumar and D. Ghose, “Sliding mode control based guidance law with impact time constraints,” presented at the American Control Conf. (ACC), 2013.
[9] D. Cho, H. J. Kim, and M.-J. Tahk, “Nonsingular Sliding Mode Guidance for Impact Time Control,” J. of Guidance, Control, and Dynamics, pp. 1-8, 2015.
[10] M. J. Tahk and D. K. Sang, “Guidance law switching logic considering the seeker's field-of-view limits,” Proc. of the Institution of Mechanical Engineers, Part G: J. of Aerospace Engineering, Vol.223, pp. 1049-1058, 2009.
[11] Y. A. Zhang, X. L. Wang, and H. L. Wu, “Impact time control guidance law with field of view constraint,” Aerospace Science and Technology, Vol.39, pp. 361-369, 2014.
[12] N. Dhananjay and D. Ghose, “Accurate Time-to-Go Estimation for Proportional Navigation Guidance,” J. of Guidance, Control, and Dynamics, Vol.37, pp. 1378-1383, 2014.

This article is published under a Creative Commons Attribution-NoDerivatives 4.0 Internationa License.

[1] [1] J. I. Lee, I. S. Jeon, and M. J. Tahk, “Guidance law to control impact time and angle,” IEEE Trans. on Aerospace and Electronic Systems, Vol.43, pp. 301-310, 2007.

[2] [2] H. Nathan and S. N. Balakrishnan, “Impact Time and Angle Guidance with Sliding Mode Control,” IEEE Trans. on Control Systems Technology, Vol.20, pp. 1436-1449, 2012.

[3] [3] Y. A. Zhang, G. X. Ma, and A. L. Liu, “Guidance law with impact time and impact angle constraints,” Chinese J. of Aeronautics, Vol.26, pp. 960-966, 2013.

[4] [4] J. Zeng, L. Dou, and B. Xin, “Cooperative salvo attack using guidance law of multiple missiles,” J. of Advanced Computational Intelligence and Intelligent Informatics (JACIII), Vol.19, pp. 301-306, 2015.

[5] [5] S. Kang and H. J. Kim, “Differential game missile guidance with impact angle and time constraints,” 18th IFAC World Congress, Milano, Italy, pp. 3920-3925, 2011.

[6] [6] I. S. Jeon, J. I. Lee, and M. J. Tahk, “Impact-time-control guidance law for anti-ship missiles,” IEEE Trans. on Control Systems Technology, Vol.14, pp. 260-266, 2006.

[7] [7] S. Zhao and R. Zhou, “Cooperative Guidance for Multimissile Salvo Attack,” Chinese J. of Aeronautics, Vol.21, pp. 533-539, 2008.

[8] [8] S. R. Kumar and D. Ghose, “Sliding mode control based guidance law with impact time constraints,” presented at the American Control Conf. (ACC), 2013.

[9] [9] D. Cho, H. J. Kim, and M.-J. Tahk, “Nonsingular Sliding Mode Guidance for Impact Time Control,” J. of Guidance, Control, and Dynamics, pp. 1-8, 2015.

[10] [10] M. J. Tahk and D. K. Sang, “Guidance law switching logic considering the seeker's field-of-view limits,” Proc. of the Institution of Mechanical Engineers, Part G: J. of Aerospace Engineering, Vol.223, pp. 1049-1058, 2009.

[11] [11] Y. A. Zhang, X. L. Wang, and H. L. Wu, “Impact time control guidance law with field of view constraint,” Aerospace Science and Technology, Vol.39, pp. 361-369, 2014.

[12] [12] N. Dhananjay and D. Ghose, “Accurate Time-to-Go Estimation for Proportional Navigation Guidance,” J. of Guidance, Control, and Dynamics, Vol.37, pp. 1378-1383, 2014.

Impact Time Control Guidance Law Considering Seeker's Field-of-View Constraint Without Time-to-Go Information

Zhe Yang†, Defu Lin, and Luyao Zang

Zhe Yang^†, Defu Lin, and Luyao Zang