Issues of Optimizing Detection of Stealth Aircraft Using Group of Satellites Flying at Different Altitudes

Authors

DOI:

https://doi.org/10.20535/RADAP.2023.93.17-21

Keywords:

stealth aircraft, detection, group flight, optimization, control function, target functionality

Abstract

The article is devoted to the optimization of the detection of stealth aircraft using a group of satellites flying at different altitudes and equipped with an infrared reproducing system. The main sources for the formation of the infrared signature of stealth aircraft are the heating of the aircraft casing during flight and the high-temperature plume emanating from the nozzle of the aircraft engine. The necessity of calculating the infrared signature of stealth aircraft is noted. The infrared signature of such aircraft is usually calculated in wide ranges of IR waves. At the same time, there are works according to which it is advisable to use narrow spectral wavelengths for these purposes. A push-pull method of detecting stealth aircraft using satellites flying in a group at different orbital altitudes has been developed. The proposed method makes it possible to increase the signal-to-noise ratio in the resulting informative signal, which is the difference between the signal from the aircraft itself and the background signal within the frame. It is shown that the introduction of a binary control signal depending on the spatial resolution of the distance to the satellites allows minimizing the total background signal coming from a group of satellites. At the same time, an increasing version of this function applied to the sum of signals from the background under a given restrictive condition ultimately increases the signal-to-noise ratio in the system, and also increases the probability of detecting a stealth aircraft using spectrometric devices installed on satellites.

Author Biographies

F. G. Agayev , Institute for Space Research of Natural Resources, National Aerospace Agency, Baku, Republic of Azerbaijan

Doctor of Technical Sciences, Professor, Director of the Institute for Space Research of Natural Resources

H. H. Asadov , Research Institute of Aerospace Information, National Aerospace Agency, Baku, Republic of Azerbaijan

Doctor of Technical Sciences, Professor, Head of Department

G. V. Aliyeva , Institute for Space Research of Natural Resources, National Aerospace Agency, Baku, Republic of Azerbaijan

Candidate of Technical Sciences, Head of Department

References

References

Zhang T., Xu Z., Wang Y., Sun F., Zhang H. (2019). Overall optimization design of high temperature components cooling coefficient for lower infrared turbofan engine. Infrared Physics & Technology, Vol. 102, 102990, doi:10.1016/j.infrared.2019.102990.

Zheng T., Dong W., Wang Z. Y., Yi X. S., Zhao Y., Yuan Z. D., Zhao Y. L. (2020). Investigation of infrared spectral emissivity of low emittance functional coating artefacts. Infrared Physics & Technology, Vol. 110, 103454, doi:10.1016/j.infrared.2020.103454.

Li N., Lv Z., Huai W., Gong G. (2016). A simulation method of aircraft plumes for real-time imaging. Infrared Physics & Technology, Vol. 77, pp. 153-161, doi:10.1016/j.infrared.2016.05.024.

Zhou Y., Wang Q., Li T., Hu H. (2017). A numerical simulation method for aircraft infrared imaging. Infrared Physics & Technology, Vol. 83, pp. 68-77, doi:10.1016/j.infrared.2017.04.011.

Chen H., Zhang H., Xi Z., Zheng Q. (2019). Modeling of the turbofan with an ejector nozzle based on infrared prediction, Applied Thermal Engineering, Vol. 159, 113910, doi:10.1016/j.applthermaleng.2019.113910.

Veiga. IV: IR Signature modelling at BAE systems ATC (2011). International Target and Background Modeling and Simulation WorkShop, ONERA, pp. 1-26.

Baranwal N., Mahulikar S. P. (2016). IR signature study of aircraft engine for variation in nozzle exit area. Infrared Physics &Technology, Vol. 74, pp. 21-27, doi:10.1016/j.infrared.2015.11.001.

Sircilli F. et. al (2015). Measurements of a micro gas turbine plume and data reduction for the purpose of infrared signature modeling. IEEE Transactions on Aerospace and Electronic System, Vol. 51, No. 4, pp. 3282-3293, DOI: 10.1109/TAES.2015.140392.

Lee J. H., Chae J. H., Ha N. K., Kim D. G., Jang H. S. (2019). Efficient Prediction of Aerodynamic Heating of a High Speed Aircraft for IR Signature Analysis. J. Korean Soc. Aeronaut. Space Sci., Vol. 47, Iss. 11, pp. 769-778, DOI:10.5139/JKSAS.2019.47.11.768.

Hu H., Li Y., Wei Z., Zheng Y. (2020). Optimization of the MSMGWB model used for the calculation of infrared remote sensing signals from hot combustion gases of hydrocarbon fuel. Infrared Physics & Technology, Vol. 107, 103286, doi:10.1016/j.infrared.2020.103286.

Gu B., Baek S. W., Jegal S. H., Choi S. M., Kim W. C. (2017). Infrared signature characteristic of a microturbine engine exhaust plume. Infrared Physics & Technology, Vol. 86, pp. 11-22, doi:10.1016/j.infrared.2017.08.014.

Kou T., Zhou Z., Liu H., Yang Y., Lu C. (2018). Multispectral radiation envelope characteristics of aerial infrared targets. Optics & Laser Technology, Vol. 103, pp. 251-259, doi:10.1016/j.optlastec.2018.01.004.

Rao G. A., Mahulikar S. P. (2012). Aircaft Powerplant and Plume Infrared Signature Modelling and Analysis. 43rd AIAA Aerospace Sciences Meeting and Exhibit, doi:10.2514/6.2005-221.

Ni, X., Yu, S., Su, X. et al. (2022). Detection spectrum optimization of stealth aircraft targets from a space-based infrared platform. Opt Quant Electron, 54, Article number: 151, doi:10.1007/s11082-021-03451-4.

Yuan H., Wang X. R., Guo B. T., Ren D., Zhang W. G., Li K. (2019). Performance analysis of the infrared imaging system for aircraft plume detection from geostationary orbit. Applied Optics, Vol. 58, Iss. 7, pp. 1691-1698, doi:10.1364/AO.58.001691.

Zhou X., Ni X., Zhang J., Weng D., Hu Z., Chen F. (2021). A Novel Detection Performance Modular Evaluation Metric of Space-based Infrared System. Research Square, doi:10.21203/rs.3.rs-989120/v1.

Elholz L. E. (1974). Differential equations and calculus of variations. M. Nauka, 432 p.

Downloads

Published

2023-09-30

How to Cite

Agayev , F. G., Asadov , H. H. and Aliyeva , G. V. (2023) “Issues of Optimizing Detection of Stealth Aircraft Using Group of Satellites Flying at Different Altitudes”, Visnyk NTUU KPI Seriia - Radiotekhnika Radioaparatobuduvannia, (93), pp. 17-21. doi: 10.20535/RADAP.2023.93.17-21.

Issue

Section

Telecommunication, navigation, radar systems, radiooptics and electroacoustics