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Application of optimal control law to laser guided bomb

Published online by Cambridge University Press:  13 March 2018

Takieddine Mouada ,
Milos V. Pavic ,
Bojan M. Pavkovic ,
Sasa Z. Zivkovic  and
Mirko S. Misljen
Takieddine Mouada*
Affiliation:
Military Academy, University of Defence, Belgrade, Serbia
Milos V. Pavic
Affiliation:
Military Technical Institute, Belgrade, Serbia
Bojan M. Pavkovic
Affiliation:
Military Technical Institute, Belgrade, Serbia
Sasa Z. Zivkovic
Affiliation:
Military Technical Institute, Belgrade, Serbia
Mirko S. Misljen
Affiliation:
Military Technical Institute, Belgrade, Serbia
*
mouadatakieddine@gmail.com
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Abstract

The paper presents a laser guided bomb guidance law based on the linear quadratic differential game theory, where a case of two perpendicular planes with two state variables in each plane has been considered. The Kalman filtering method has been used for noise removal from the measured signals and for estimation of the missing state variable values needed for the optimal guidance law. Optimisation has been conducted with respect to minimisation of the performance index. Comparative analysis of different guidance laws is done. A statistical analysis is performed to obtain the terminal miss distance in dependence on total flight time.

Keywords

Proportional navigationoptimal guidancemissile controlline-of-sight rate estimationlaser guided bombKalman filterstrap-down seeker

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 122 , Issue 1251 , May 2018 , pp. 785 - 797
Copyright
Copyright © Royal Aeronautical Society 2018 

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References

REFERENCES

1. Delong, F., Suochang, Y. and Yingxi, L. Research on missile system with strapdown guidance technology, Advanced Materials Research, 2013, 785–786, pp 1560-1563.Google Scholar
2. Yao, J., Wei Zhou, F. and Wang, X. Study of increment proportional guidance law for high maneuvering target, Int J Signal Processing, Image Processing and Pattern Recognition, 2015, 8, (6), pp 181-192.Google Scholar
3. David, K. and Solomon, R. Performance evaluation of proportional navigation guidance for low-maneuvering targets, Int J Scientific & Engineering Research, 2014, 5, (9), pp 93-98.Google Scholar
4. Pavkovic, B., Pavic, M. and Cuk, D. Frequency-modulated pulse-jet control of an artillery rocket, J Spacecraft and Rockets, 2012, 49, (2), pp 286-294.Google Scholar
5. Kun, C.-C., Chiang, F.-L. and Chen, K.-Y. Design a three-dimensional pursuit guidance law with feedback linearization method, Int J Aerospace and Mech Engineering, 2011, 5, (7), pp 289-293.Google Scholar
6. Dowan, K., Chang-Kyung, R., Yongho, K. and Jongju, K. Guidance and control for missiles with a strapdown seeker, Proceedings of the 11th International Conference on Control, Automation and Systems, October 2011, KINTEX, Gyeonggi-do, Korea.Google Scholar
7. Jwo, D.-J., Shih, J.-H., Hsu, C.-S. and Yu, K.-L. Development of a strapdown inertial navigation system simulation platform, J Machine Science and Technology, 2014, 22, (3), pp 381-391.Google Scholar
8. Sun, T., Chu, H., Zhang, B., Jia, H., Guo, L., Zhang, Y. and Zhang, M. Line-of-sight rate estimation based on UKF for strapdown seeker, Hindawi Publishing Corporation Mathematical Problems in Engineering, 2015, 2015, (14) pp 1-14.Google Scholar
9. Tapas, A., Rao, V. and Prabhakar, N. Adaptive estimation of line-of-sight rate measurement from a radio frequency seeker, Defence Science J, 2005, 55, (3), pp 307-312.Google Scholar
10. Ben-Asher, J.Z. Linear quadratic pursuit-evasion games with terminal velocity constraints, J Guidance, Control, and Dynamics, 1996, 19, (2), pp 499-501.CrossRefGoogle Scholar
11. Grewal, M.S. and Andrews, , A.P. Kalman Filtering: Theory and Practice Using MATLAB, 4th ed., Wiley-IEEE Press, 2014.Google Scholar
12. Zarchan, P. Tactical and strategic missile guidance, Progress in Astronautics and Aeronautics, 6th ed, American Institute of Aeronautics and Astronautics, 2012.Google Scholar