High-precision assessment of the initial orientation of drone aircraft by satellite measurements
https://doi.org/10.46973/0201-727x_2023_4_54
Abstract
The paper deals with the problem of the initial orientation of the drone aircraft by high-precision satellite measurements. The solution is obtained in the form of explicit dependencies of the orientation angles of the UAV relative to the geographical coordinate system from secondary satellite measurements of the coordinates of navigation receivers located on the drone aircraft in the geocentric coordinate system. It is given a numerical estimate of the proposed method ‘precision illustrating the effectiveness of its practical application.
About the Authors
S. V. Sokolov
Rostov State University of Economics (RSUE)
Russian Federation
Russian Federation
Sokolov Sergey Viktorovich, Doctor of Engineering Sciences, Professor, Head of the Scientific-Production Laboratory
A. V. Kostyukov
Rostov State Transport University (RSTU)
Russian Federation
Russian Federation
Kostyukov Alexander Vladimirovich, Chair «Theoretical Foundations of Electrical Engineering», Candidate of Engineering Sciences, Associate Professor
E. N. Tishchenko
Rostov State University of Economics (RSUE)
Russian Federation
Russian Federation
Tishchenko Evgeny Nikolaevich, Faculty «Computer Technologies and Information Security», Doctor of Economics Sciences, Professor, Dean
References
1. Sokolov, S. V. Stochastic estimation, control and identification in high-precision navigation systems / S. V. Sokolov, V. A. Pogorelov // Rostov-on-Don Scientific Research Institute of Radio Communications. – Moscow : LLC Publishing company «Physico-mathematical literature», 2016. – 264 p. – ISBN 978-5-9221-1672-5.
2. Perov, A. I. Glonass. Principles of construction and functioning / A. I. Perov, V. N. Kharisov. – Ed. 4th, reprint. and add. – Moscow : Radio Engineering, 2010. –800 p. – ISBN 5-93108-076-77.
3. Anuchin, O. N. Integrated orientation and navigation systems for marine mobile objects / O. N. Anuchin, G. I. Emeliantsev ; under the general editorship of V. G. Peshekhonov // State Scientific Center of the Russian Federation. Federation – Center. scientific-research. in-t «Electrical appliance». – 2nd Ed., reprint. and add. – Saint. Petersburg : SSC RF – Central Research Institute «Electropribor», 2003. – 389 p. – ISBN 5- 900780-47-3.
4. Tikhonov, V. I. Statistical analysis and synthesis of radio engineering devices and systems : manual for students of radio engineering universities specialties / V. I. Tikhonov, V. N. Kharisov. – 2nd ed., ispr. – Moscow : Radio and Communications, 2004. – ISBN 5-256-01701-2.
5. Pogorelov, V. A. Solving the problem of close integration of satellite and inertial platform navigation systems / V. A. Pogorelov, S. V. Sokolov // Space research. – 2015. – Vol. 53, No. 6. – P. 497. – DOI 10.7868/S0023420615060059.
6. Kleusberg, А. Mathematics of Attitude Determination with GPS / А. Kleusberg // GPS WORLD. – 1995. – No. 9. – P. 72–78. – ISSN 1048-5104.
7. Graas, F. GPS Interferometric Attitude and Heading Determination : Initial Flight Test Results / F. Graas, Van, M. S. Braasch // Navigation : Journal of the Institute of Navigation : 1991– 1992. – No. 38 (4). – P. 279–316.
8. Nadler, A. An Efficient Algorithm for Attitude Determination Using GPS. ION GPS-98 / A. Nadler, I. Y. Bar-Itzhack. – 1998. – P. 1783–1789.
9. Octopus : Multi antennae GPS/GLONASS RTK System. ION GPS-2000 / L. Rapoport, I. Barabanov, A. Khvalkov [et al.]. – P. 797–804.
10. Euler, H.-J. Attitude determination : Exploiting all Information for Optimal Ambiguity Resolution. ION GPS-95 / H.-J. Euler, C. Hill. – P. 1751–1757.
11. On improving the accuracy of a GPS compass for small-sized objects / G. I. Emeliantsev, A. P. Stepanov, B. A. Blazhnov [et al.] // Gyroscopy and navigation. – 2015. – No. 1 (88). – P. 18–28. – DOI 10.17285/0869-7035.2015.23.1.018-029.
12. Shakhin, E. M. Mathematical analysis of phase errors in the GPS receiver tracking scheme with interference of various kinds / E. M. Shakhin // Gyroscopy and navigation. – 2018. – Vol. 26, No. 3 (102). – P. 40–53. – DOI 10.17285/0869-7035.2018.26.3.040-053.
13. Mitrakhovich, I. O. System for determining the angles of orientation of objects in space based on the RTK method / I. O. Mitrakhovich // International Congress on Informatics : Information systems and Technologies: materials of the International Scientific Congress, Minsk, October 24–27, 2016 / S. V. Ablameyko (editor-in-chief). – Minsk : Belarusian State University, 2016. – P. 46–51. – EDN XWMSEF.
14. Tyapkin, V. N. Methods for determining the navigation parameters of mobile vehicles using the GLONASS satellite radio navigation system / V. N. Tyapkin, E. N. Garin. – Krasnoyarsk : Siberian Federal University, 2012. – 259 p. – ISBN 978-5-7638-2639-5.
15. Emeliantsev, G. I. On the initial exhibition and evaluation of errors of the BINC measuring module using satellite phase measurements / G. I. Emeliantsev, A. P. Stepanov, B. A. Blazhnov // Gyroscopy and navigation. – 2019. – Vol. 27, No. 1 (104). – P. 47–60. – DOI 10.17285/0869-7035.2019.27.1.047-060.
16. Interface Control Document: NAVSTAR GPS Space Segment / Navigation User Interfaces (ICDGPS-200). Rockwell Int. Corp., 1987.3427.
17. Lukasevich, V. I. Algorithm for estimating the rotation parameters of a distributed antenna by satellite measurements / V. I. Lukasevich, V. A. Pogorelov, S. V. Sokolov // Radio Engineering. – 2015. – No. 6. – P. 122–131. – ISSN 0033-8486.
18. Error estimation and selection of inertial navigation system parameters for uncoupled integration with multi-antenna systems / D. Kaleev, A. Pereverzev, Y. Savchenko, A. Silantiev // Proceedings of the 2016 IEEE North West Russia Section Young Researchers in Electrical and Electronic Engineering Conference, EIConRusNW 2016, Saint Petersburg, 02–03 февраля 2016 года. – Saint Petersburg, 2016. – P. 414–417. – DOI 10.1109/EIConRusNW.2016.7448209.
19. Shakhin, E. M. Mathematical analysis of phase errors in the GPS receiver tracking scheme with interference of various kinds / E. M. Shakhin // Gyroscopy and navigation. – 2018. – Vol. 26, No. 3 (102). – P. 40–53. – DOI 10.17285/0869- 7035.2018.26.3.040-053.
Review
For citations:
Sokolov S.V., Kostyukov A.V., Tishchenko E.N. High-precision assessment of the initial orientation of drone aircraft by satellite measurements. Vestnik Rostovskogo Gosudarstvennogo Universiteta Putej Soobshcheniya. 2023;(4):54-61. (In Russ.) https://doi.org/10.46973/0201-727x_2023_4_54
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