Preview

Mekhatronika, Avtomatizatsiya, Upravlenie

Advanced search
Open Access Open Access  Restricted Access Subscription or Fee Access

Planning the Optimal Reference Flight Path of an Aircraft Using a Terrain Map

https://doi.org/10.17587/mau.24.496-502

Abstract

In connection with the development of aviation technology, the expansion of the functionality of modern aircraft and the complication of the tasks being solved, additional stringent requirements are imposed on the accuracy of air navigation. Along with high accuracy, navigation autonomy is also required. The autonomy of aircraft navigation implies the navigation of an aircraft without the use of active radar facilities. In this article, to calculate the optimal reference flight path of an aircraft in a horizontal plane, the Bellman dynamic programming method is proposed using a digital terrain map. A technique, algorithms have been developed, and a numerical experiment has been carried out using fragments of a digital terrain map. High accuracy and autonomy of navigation are necessary, among other things, to ensure stealth (invisibility) of aircraft by ground-based radar facilities of a potential enemy in low-altitude flight mode. The best stealth of an aircraft flight in a low-altitude flight mode is achieved not only by flying around, but also by avoiding obstacles, due to the shielding properties of the earth’s surface. Autonomy of navigation provides periodic correction of the reference flight path during long-term flight, and high accuracy prevents aircraft collisions with the earth’s surface in low-altitude flight mode. The purpose of this work is to select the optimal reference trajectory (route) of an aircraft flight in the low-altitude flight mode. This article discusses a method developed based on the principle of dynamic programming for calculating the reference flight path in the horizontal plane depending on the DEM and the implementation of the algorithm based on the proposed method with a specific numerical example. The method makes it possible to calculate the optimal flight route, which provides the greatest secrecy of the aircraft in the low-altitude flight mode using the screening properties of the earth’s surface irregularities. 

About the Authors

N. B. Agayev
Ministry of Science and Education of the Republic of Azeribaijan, Institute of Information Technology;
Azerbaijan

 Baku



Q. H. Orujov
2National Aviation Academy of AZAL CJSC
Azerbaijan

 Baku



N. N. Kalbiyev
National Aviation Academy of AZAL CJSC
Azerbaijan

 Baku



References

1. Beloglazov I. N., Dzhandzhgava G. I., Chigin G. P. Fundamentals of navigation in geophysical fields, Moscow, Nauka, 1985 (in Russian).

2. Özdemir C. Mersin University Inverse synthetic aperture radar imaging with MATLAB (Wiley series in microwave and optical engineering), Includes bibliographical references, Singapore, 2012.

3. Kassaei S. l., Kosari A. Aircraft Trajectory Planning with an Altitude-Bound in terrain-following flight, Modares Mechanical Engineering, 2018, 17, pp. 135—144 (in Persian), available at: https://www.researchgate.net/publication/321462018.

4. Menon P. K. A., Kim E., Cheng V. H. L. Optimal trajectory synthesis for terrain-following flight. Journal of Guidance, Control, and Dynamics, 1991, vol. 14, no. 4, pp. 807—813, available at:https://doi.org/10.2514/3.20716.

5. Sun L., Li S., Wang D., ZhaoX., Li X. Flight route planning for terrain navigation using multi-fractal theory, Journal of Tsinghua University, 2011, vol. 51, available at: https://www. researchgate.net/ publication/289437769.

6. Flood C. Real-time Trajectory Optimization for Terrain Following Based on Non-linear Model Predictive Control [Electronic resource], Linköping, 2001, available at: http://www.divaportal.org/smash/get/diva2: 17767/FULLTEXT01.pdf.

7. Leondes K. T. Modern theory of control systems, Moscow, Science, 1970 (in Russian).

8. Wentzel E. S. Operations research. Tasks. Principles, methodology, Moscow, Science, 1988 (in Russian).

9. Moiseev N. N. et al. Optimization Methods, Moscow, Science, 1978 (in Russian).

10. Boltyansky V. G. Mathematical Methods for Optimal Control of Discrete Systems, Moscow, Science, 1966 (in Russian).

11. Marchuk G. I. Methods of computational mathematics, Moscow, Science, 1989 (in Russian).

12. Alekseev O. G. Complex application of discrete optimization methods, Moscow, Science, 1987 (in Russian).

13. Krasovsky A. A. Reference on the theory of automatic control, M.: Science, 1987. (in Russian)

14. Leshchenko S. P., Baturinsky M. P., Svistunov D. Yu. Method for calculating the optimal trajectory of the flight of air objects according to the criterion of minimum detection probability. UDC 621.396, ISSN 1681-7710, Information processing systems, 2005, iss. 2 (42) (in Russian).

15. Melnikov A. V., Korobkin D. I., Rogozin E. A. Calculation and selection of the optimal flight path of an unmanned aerial vehicle when observing ground objects, available at: https://www. elibrary.ru/item.asp?id=27250327 (in Russian).

16. Ishchuk I. N., Likhachev M. A. Modeling of the optimal flight route for unmanned aerial vehicles based on infrared video navigation data based on the modernized Dijkstra algorithm, Zh. Sib. feder. university Engineering and technology, 2021, vol. 14, no. 7, pp. 788—802, DOI: 10.17516/1999-494X-0356 (in Russian).

17. Nikiforova L. N. Optimal control in constructing helicopter flight trajectories to a given point in space, Program Systems: Theory and Applications, 2012, vol. 3, iss. 2, pp. 61—75 (in Russian).

18. Sharma T. Optimum Flight Trajectories for Terrain Collision, Royal Melbourne Institute of Technology, 2006, pp. 1—155, available at: https://core.ac.uk/download/pdf/18619455.pdf.


Review

For citations:


Agayev N.B., Orujov Q.H., Kalbiyev N.N. Planning the Optimal Reference Flight Path of an Aircraft Using a Terrain Map. Mekhatronika, Avtomatizatsiya, Upravlenie. 2023;24(9):496-502. (In Russ.) https://doi.org/10.17587/mau.24.496-502

Views: 407


ISSN 1684-6427 (Print)
ISSN 2619-1253 (Online)