Geodesic
Modeling of kinematic characteristics of a mobile antenna of a spacecraft in a two-stage pivoting device
Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, Tome 29 (2023) no. 4, pp. 125-132 Cet article a éte moissonné depuis la source Math-Net.Ru

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The problem of calculating the kinematic characteristics of a mobile antenna device (AD) based on the specified values of kinematic characteristics of the line of sight (LS) "spacecraft — information reception point" in the associated coordinate system of the spacecraft is considered. The kinematic characteristics of the AD in the form of the current values of its rotation angles and angular velocities and accelerations (according to the corresponding control channels) are determined from the conditions for combining the LS with the axis of the directional diagram of the AD for the case of a two-stage pivoting device with mutually orthogonal axes of rotation of the AD.
Keywords: spacecraft, pivot device, kinematic characteristics, line of sight, control channels.
Mots-clés : mobile antenna 
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     title = {Modeling of kinematic characteristics of a mobile antenna of a spacecraft in a two-stage pivoting device},
     journal = {Vestnik Samarskogo universiteta. Estestvennonau\v{c}na\^a seri\^a},
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Yu. N. Gorelov; L. V. Kurganskaya. Modeling of kinematic characteristics of a mobile antenna of a spacecraft in a two-stage pivoting device. Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, Tome 29 (2023) no. 4, pp. 125-132. http://geodesic.mathdoc.fr/item/VSGU_2023_29_4_a6/

[1] Gorelov Yu.N., Kurgankaya L.V., “Modeling of kinematic characteristics of the line of sight of a mobile antenna of a spacecraft when it is pointed at an information reception point”, Vestnik Samarskogo Universiteta. Estestvennonauchnaya Seriya Vestnik of Samara University. Natural Science Series, 29:4 (2023), 77–84 (In Russ.) | MR

[2] Gorelov Yu.N., Gorelova O.I., Manturov A.I., “Modeling of kinematic characteristics of a controlled mobile antenna of a spacecraft”, Motion control and navigation of aircraft, proceedings of the XI All-Russian research and technical seminar on motion control and navigation of aircraft (June, 23–25, 2003, Samara, Russian Federation), Samara, 2003, 68–73 (In Russ.)

[3] Strazheva I.V., Melkumov V.S., Vector-matrix methods in flight mechanics, Mashinostroenie, M., 1973, 260 pp. (In Russ.)

[4] Kirilin A.N., Anshakov G.P., Akhmetov R.N., Storozh A.D., Spacecraft engineering. Scientific and technical research and practical developments of the State Research and Production Space-Rocket Center “TsSKB-Progress”, Samara, 2017, 376 pp. (In Russ.)