The Earth Orientation Parameters Inaccuracy and Spacecraft Motion Prediction Errors. 2. GPS Satellites
Author:
Publisher
Allerton Press
Subject
Industrial and Manufacturing Engineering,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.3103/S1068798X20120370.pdf
Reference9 articles.
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2. Kozorez, D.A., Krasil’shchikov, M.N., and Kruzhkov, D.M., Computer simulation of the spacecraft insertion process into geostationary orbit by electric propulsion system, Vestn. Komp’yut. Inf. Tekhnol., 2015, no. 9, pp. 9–15.
3. Voiskovskii, A.P., Kozorez, D.A., Krasilshchikov, M.N., and Kruzhkov, D.M., Autonomous navigation during the final ascent of a spacecraft into the geostationary orbit. I. Simulation of operation of an integrated autonomous SC navigation and control system, J. Comput. Syst. Sci. Int., 2016, vol. 55, no. 5, pp. 785–795.
4. Akimov, E.V., Kruzhkov, D.M., and Yakimenko, V.A., High-precision simulation of onboard signal receivers in global navigation systems, Russ. Eng. Res., 2020, vol. 40, no. 2, pp. 152–155.
5. Akimov, E.V., Kruzhkov, D.M., and Yakimenko, V.A., Prototype information system for high-precision navigation in global satellite systems, Russ. Eng. Res., 2020, vol. 40, no. 2, pp. 156–159.
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