Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter

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 g...

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Main Authors: V. M. Ananenko, A. D. Golyakov, P. V. Kalabin
Format: Article
Language:English
Published: Samara National Research University 2020-07-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/7901/7736
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spelling doaj-a89326c76c1049618880d0199a6396382021-08-25T08:10:24ZengSamara National Research UniversityВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение2542-04532541-75332020-07-0119271810.18287/2541-7533-2020-19-2-7-187367Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filterV. M. Ananenko0A. D. Golyakov1P. V. Kalabin2Mozhaisky Military Space AcademyMozhaisky Military Space AcademyMozhaisky Military Space AcademyA 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 Keplers 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 robots 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.https://journals.ssau.ru/vestnik/article/viewFile/7901/7736space robotmethods of autonomous navigationonboard optical and electronic meanskepler’s elements of the orbitautonomous navigation systemorbital angular velocitymotion parameters
collection DOAJ
language English
format Article
sources DOAJ
author V. M. Ananenko
A. D. Golyakov
P. V. Kalabin
spellingShingle V. M. Ananenko
A. D. Golyakov
P. V. Kalabin
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
space robot
methods of autonomous navigation
onboard optical and electronic means
kepler’s elements of the orbit
autonomous navigation system
orbital angular velocity
motion parameters
author_facet V. M. Ananenko
A. D. Golyakov
P. V. Kalabin
author_sort V. M. Ananenko
title Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
title_short Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
title_full Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
title_fullStr Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
title_full_unstemmed Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
title_sort method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
publisher Samara National Research University
series Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
issn 2542-0453
2541-7533
publishDate 2020-07-01
description 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 Keplers 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 robots 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.
topic space robot
methods of autonomous navigation
onboard optical and electronic means
kepler’s elements of the orbit
autonomous navigation system
orbital angular velocity
motion parameters
url https://journals.ssau.ru/vestnik/article/viewFile/7901/7736
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