Оцінювання параметрів відносного руху некооперованого космічного апарата за візуальною інформацією
| Сальніков, ММ, 1Мельничук, СВ, 1Губарев, ВФ, Максимюк, ЛВ, Шевченко, ВМ 1Інститут космічних досліджень Національної академії наук України і Державного космічного агентства України, Київ |
| Косм. наука технол. 2023, 29 ;(3):16-23 |
| https://doi.org/10.15407/knit2023.03.016 |
| Язык публикации: Англійська |
Аннотация: Розглянуто задачу визначення параметрів відносного руху некооперованого космічного апарату (НКА), що знаходиться у вільному некерованому русі, за результатами вимірювання відстані до цього апарату та його кватерніону орієнтації. Припускається, що ці виміри виконуються системою технічного зору (СТЗ). Конкретний тип СТЗ не розглядається. Припускається, що СТЗ вимірює відстань та положення так званої графічної системи координат, яка жорстко закріплена на НКА. До параметрів відносного руху відносяться вектор відстані до центру мас (ц.м.) НКА, кватерніон орієнтації головних осей інерції НКА відносно системи координат СТЗ, кватерніон орієнтації графічної системи координат щодо головної системи координат НКА, відношення моментів інерції, вектор положення ц.м. у графічній системі координат.
Задача вирішується за допомогою динамічного фільтра, заснованого на методі еліпсоїдального оцінювання. Метод передбачає знання лише максимальних значень шуму вимірів, стохастичні характеристики шуму не передбачаються відомими і тому не використовуються. Властивості запропонованого алгоритму було продемонстровано за допомогою чисельного моделювання. Отримані результати планується використовувати для розробки, створення та випробування навігаційної системи зближення та стикування сервісного космічного апарату, що розробляється групою підприємств космічної галузі України під керівництвом ТОВ «Курс-Орбітал».
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| Ключевые слова: відеозображення, космічний апарат, оцінювання, параметри відносного руху |
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https://doi.org/10.1016/S1000-9361(09)60206-5
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https://doi.org/10.1109/AERO.2019.8742148
24. Liang H., Wang J., Wang Y., Huo W. Monocular-vision-based spacecraft relative state estimation under dual number algebra. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. (2020). vol. 234, pp. 221 - 235.
https://doi.org/10.1177/0954410019864754
25. Ivanov D. S., Karpenko S. O., Ovchinnikov M. Ju., Sakovich M. A. Relative motion determination of satellites at their separation on results of videoimages processing, Preprinty IPM im. M. V. Keldysha[Preprints of Keldysh IAM]. (2012), No. 057, 24 p.
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27. Grishin V.A., Zhukov B.S. Peculiarities of image recognition at its application to relative navigation tasks at spacecraft docking. Modern problems of Earth Remote Control. (2020). Vol. 17, No 7. pp. 58-66.
https://doi.org/10.21046/2070-7401-2020-17-7-58-66
28. Molina Saqui J.C., Tkachev S.S. Kalman filter application for the angular motion estimation by video processing. Keldysh IAM Preprints. (2021). No. 27. 27 p.
https://doi.org/10.20948/prepr-2021-27-e
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https://doi.org/10.1201/9781003337010-12
31. Volosov V., Salnikov N., Melnychuk S., Shevchenko V. Control Synthesis of Rotational and Spatial Spacecraft Motion at Approaching Stage of Docking. Chapter 12 in the book "Advanced Control Systems: Theory and Applications". (2021). River Publishers Series in Automation, Control and Robotics. pp.331-364.
https://doi.org/10.1201/9781003337010-14
32. Koshkin N., Melikyants S., Korobeinikova E., Shakun L., Strakhova S., Kashuba V., Romanyuk Ya., Terpan S. Simulation of the orbiting spacecraft to analysis and understand their rotation based on photometry. Odessa Astronomical Publications. (2019). vol. 32, pp.158-161.
https://doi.org/10.18524/1810-4215.2019.32.183899
33. Koshkin N., Shakun L., Kozhukhov O., Kozhukhov D., Mamarev V., Prysiaznyi V., Ozeryan A., Bilinsky A., Kudak V., Neubauer I. Simultaneous multi-site photometry of LEO satellites for rotation characterization. Proceedings of the 8th European Conference on Space Debris. (2021). Darmstadt, Germany, 20-23 April 2021.
http://conference.sdo.esoc.esa.int.
34. Sarychev V.A., Paglione P., Guerman A.D. Stability of Equilibria for a Satellite Subject to Gravitational and Constant Torques. Journal of Guidance Control and Dynamics. (2008). vol. 31. № 2. P. 386-394.
https://doi.org/10.2514/1.28753
35. Markley, F.L., Crassidis, J.L. Fundamentals of Spacecraft Attitude Determination and Control. New York: Springer Science+Business Media, 2014.
https://doi.org/10.1007/978-1-4939-0802-8
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