The rendezvous of two spacecraft (passive and active) using a tether system is studied. Two laws of the tether control are proposed to ensure the safe rendezvous of bodies. A minimum allowable thrust of the active spacecraft and the parameters of the tether control laws are defined, under which the rendezvous is implemented safe. Based on the results of numerical simulation, the ability to control the tether using the proposed laws is showed.
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Jasper, L.E., Seubert, C.R., Schaub, H., Trushkyakov, V., and Yutkin, E., Tethered Tug for Large Low Earth Orbit Debris Removal, Proc. of the 22nd AAS/AIAA Space Flight Mechanics Meeting “Spaceflight Mechanics 2012”, Charleston, 2012, vol. 143, Advances in the Astronautical Sciences, AAS 12–252.
Afanas’ev, V.A., Degryarev, G.L., and Meshchanov, A.S., Rocket Berthing to an Asteroid: Design Problem, Izv. Vuz. Av. Tekhnika, 2013, vol. 56, no. 2, pp. 72–77 [Russian Aeronautics (Engl. Transl.), vol. 56, no. 2, pp. 199–207].
Beletskii, V.V. and Levin, E.M., Dinamika kosmicheskikh trosovykh system (Dynamics of Space Tether Systems), Moscow: Nauka, 1990.
Morozov, L.V., Maneuvering in the Vertical Plane of a Flight Vehicle Towed by Cable Connection, Izv. Vuz. Av. Tekhnika, 2005, vol. 48, no. 4, pp. 3–6 [Russian Aeronautics (Engl. Transl.), vol. 48, no. 4, pp. 1–7].
Aslanov, V.S. and Ledkov, A.S., Dynamics of the Tethered Satellite System, Cambridge: Woodhead Publishing Limited, 2012.
Lee, J. and Schaub, H., Tethered Towing Using Open-Loop Input-Shaping and Discrete Thrust Levels, Acta Astronautica, 2014, vol. 105, issue. 1, pp. 373–384.
DeLuca, L.T., Bernelli, F., Maggi, F., Tadini, P., Pardini, C., Anselmo, L., Grassi, M., Pavarin, D., Francesconi, A., Branz, F., Chiesa, S., Viola, N., Bonnal, C., Trushlyakov, V., and Belokonov, I., Active Space Debris Removal by a Hybrid Propulsion Module, Acta Astronautica, 2013, vol. 91, no. 1, pp. 20–33.
This work was supported by the Ministry of Education and Science of the Russian Federation, contract no. 9.549.2014/K.
Russian Text © The Author(s), 2020, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 1, pp. 156–160.
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Aslanov, V.S., Pikalov, R.S. & Gunchin, E.R. Control of the Rendezvous of Two Spacecraft Using a Tether System. Russ. Aeronaut. 63, 171–175 (2020). https://doi.org/10.3103/S1068799820010249
- space tether system
- rendezvous of spacecraft
- space debris