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SPACECRAFT ORBITAL STABILITY VS TOTAL SOLAR IRRADIANCE ArticleYefremov Alexander P., Vorobyeva Alexandra A.Acta Astronautica. Том 235. 2025. С. 759-765
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SATURATED OUTPUT FEEDBACK CONTROL OF FREE-FLOATING SPACE MANIPULATOR WITH FRAGILITY-AVOIDANCE PRESCRIBED PERFORMANCE ArticleZhou H., Zhuang H., Shen Q., Razoumny V.Y., Razoumny Y.N., Wu S.Acta Astronautica. Том 228. 2025. С. 972-984
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TWO-STAGE 'SLINGSHOT AMPLIFIER' CAN DETECT SUBTLE GRAVITATIONAL DEVIATIONS ArticleYefremov A.P., Vorobyeva A.A.Acta Astronautica. Том 220. 2024. С. 462-468
TWO-STAGE ‘SLINGSHOT AMPLIFIER’ CAN DETECT SUBTLE GRAVITATIONAL DEVIATIONS ArticleYefremov A.P., Vorobyeva A.A.Acta Astronautica. Том 220. 2024. С. 462-468
MACHINE LEARNING METHODS FOR MODELING THE KINETICS OF COMBUSTION IN PROBLEMS OF SPACE SAFETY ArticleMalsagov M.Y., Mikhalchenko E.V., Karandashev I.M., Stamov L.I.Acta Astronautica. Том 225. 2024. С. 656-663
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PROMISING METHOD FOR IMPROVING THE ACCURACY OF ESTIMATES IN SPACE DEBRIS TASKS - OPTIMAL FILTERING OF MEASUREMENTS ArticleUsovik I.V., Nazarenko A.I.Acta Astronautica. 2023. С. 826-830
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