Email this article 
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
- Authors: Ananenko V.M.1, Golyakov A.D.1, Kalabin P.V.1
-
Affiliations:
- Mozhaisky Military Space Academy
- Issue: Vol 19, No 2 (2020)
- Pages: 7-18
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/7901
- DOI: https://doi.org/10.18287/2541-7533-2020-19-2-7-18
- ID: 7901
Cite item
Full Text
Abstract
A method of preliminary solution of the problem of space robot navigation based on the results of measurements carried out using its onboard optronic equipment is presented. The initial data of the navigation problem are the directional cosines of the space robot orientation vector in the absolute geocentric equatorial coordinate system with reference to time during one revolution. Analytical expressions are obtained for determining unknown parameters of the motion of the space robot center of mass in the form of Kepler’s elements of the orbit. It is shown that to determine the right ascension of the ascending node, the inclination and the semi-major axis of the orbit of the space robot, information about the orientation of its radius vector at various times is used, and to determine the perigee argument, the moment of passing the perigee and the eccentricity of the orbit, the angular orbital speed of the space robot is used, which is determined by the results of evaluating the speed of change in the orientation of its radius vector over time. The presented results can be used in the development of software for navigation systems that allow autonomous determination of the parameters of the space robot’s orbit using onboard electro-optical sensors in the absence of a priori information about the parameters of the reference orbit or signals from satellite radio navigation systems.
About the authors
V. M. Ananenko
Mozhaisky Military Space Academy
Author for correspondence.
Email: avm-brok@mail.ru
Candidate of Science (Engineering), Associate Professor,
Senior Lecturer of the Department of Autonomous Control Systems
A. D. Golyakov
Mozhaisky Military Space Academy
Email: algol1949@mail.ru
Doctor of Science (Engineering), Professor,
Professor of the Department of Autonomous Control Systems
P. V. Kalabin
Mozhaisky Military Space Academy
Email: kalabinpavel179@gmail.com
Adjunct
Russian FederationReferences
- Silantyev S., Fominov I., Korolev S. Robots in orbit. Aerospace Sphere Journal. 2016. No. 2 (87). P. 118-123. (In Russ.)
- Akim E.L., Kapralov M.A., Stepaniants V.A., Tuchin A.G., Tuchin D.A. Parameter determination of the spacecraft by the onboard navigation system on measurements of doppler and pseudorange of space satellite systems. Keldysh Institute. Preprints. 2004. No. 20. 25 p. (In Russ.)
- Mikhailov N.V. Avtonomnaya navigatsiya kosmicheskikh apparatov pri pomoshchi sputnikovykh radionavigatsionnykh system [Autonomous navigation of space vehicles with GNSS]. SPb: Politekhnika Publ., 2014. 362 p.
- Tuchin D.A. Autonomous spacecraft's on-board orbit determination. Keldysh Institute. Preprints. 2019. No. 7. 36 p. (In Russ.). doi: 10.20948/prepr-2019-7
- Filimonov V.A., Tislenko V.I., Lebedev V.Yu., Kravets A.P. Sigma Point Algorithm of the Kalman Filter in Spacecraft Autonomous Navigation. Rocket-Space Device Engineering and Information Systems. 2017. V. 4, no. 1. P. 3-7. (In Russ.). doi: 10.17238/issn2409-0239.2017.1.3
- Andronov V.G., Emelyanov S.G. Method of autonomous navigating spacecraft. Proceedings of the Southwest State University. 2016. No. 2 (65). P. 65-73. (In Russ.)
- Anshakov G.P., Golyakov A.D., Petrishchev V.F., Fursov V.A. Avtonomnaya navigatsiya kosmicheskikh apparatov [Spacecraft autonomous navigation]. Samara: Space Rocket Center «Progress» Publ., 2011. 486 p.
- Treshchalin A. P. The use of spacecraft opto-electronic devices for preliminary orbit determination of near-Earth objects. Proceedings of MIPT. 2012. V. 4, no. 3 (15). P. 122-131. (In Russ.)
- Porfir'ev L.F., Smirnov V.V., Kuznetsov V.I. Analiticheskie otsenki tochnosti avtonomnykh metodov opredeleniya orbit [Analytical assessment of the accuracy of autonomous orbit determination methods]. Moscow: Mashinostroenie Publ., 1987. 280 p.
- Avanesov G.A., Bessonov R.V., Dementiev V.Yu. Results of software tests of the star tracker BOKZ-M60/1000 on dynamic test bench. Sovremennye Problemy Distantsionnogo Zondirovaniya Zemli iz Kosmosa. 2013. V. 10, no. 4. P. 24-33. (In Russ.)
- Gandlevsky Yu.M., Mikhailov E.N., Mosolova Yu.S., Rabovsky A.E. Assessment of infrared local vertical sensors based on flight test results. Electromechanical Matters. VNIIEM Studies. 2014. V. 141, no. 4. P. 31-38. (In Russ.)
- El'yasberg P.E. Vvedenie v teoriyu poleta iskusstvennykh sputnikov Zemli [Introduction to the theory of flight of artificial earth satellites]. Moscow: Nauka Publ., 1965. 540 p.
- Sergienko A.B. Tsifrovaya obrabotka signalov [Digital signal processing]. SPb.: Piter Publ., 2003. 604 p.
- Medvedeva K.S., Berdnikov G.S. Comparison of a low-frequency Butterworth filter with a radially symmetric SE-filter. Proceedings of the IV International Conference «Information technologies and nanotechnologies» (ITNT-2018) (April, 24-27, 2018, Samara, Russian Federation). Samara: Novaya Tekhnika Publ., 2018. P. 745-751. (In Russ.)
- Fominov I.V., Korolev S.U., Zotkin M.U. Theoretical approaches to the creation of an integrated navigation system with adaptive of complex information processing. Proceedings of the Military Space academy named after A.F. Mozhaisky. 2015. No. 646. P. 68-76. (In Russ.)
Supplementary files
