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Publications in Math-Net.Ru |
Citations |
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2018 |
| 1. |
B. I. Zhukov, V. V. Sazonov, Yu. G. Sikharulidze, V. S. Yaroshevskiy, “«Luna-Glob» spacecraft attitude motion control in the mode of the constant solar orientation”, Keldysh Institute preprints, 2018, 238, 28 pp.   |
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| 2. |
Yu. G. Sikharulidze, A. N. Korchagin, A. S. Samotokhin, A. G. Tuchin, “Terminal control algorithm for descent from near-Earth orbit with landing in given region”, Keldysh Institute preprints, 2018, 046, 27 pp. |
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2008 |
| 3. |
Yu. G. Sikharulidze, B. I. Zhukov, “Dynamic loadings on the carrier aircraft at implementation of the vehicle air launch (the four-basic scheme)”, Keldysh Institute preprints, 2008, 064, 34 pp. |
| 4. |
Yu. G. Sikharulidze, B. I. Zhukov, “Dynamic loadings on the carrier aircraft at implementation of the vehicle air launch (the two-basic scheme)”, Keldysh Institute preprints, 2008, 009, 24 pp. |
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2005 |
| 5. |
A. V. Borisov, R. K. Ivanov, Yu. G. Sikharulidze, “Analysis of gusts at the vertical maneuver phase (“Pitchover”) of the carrier-aircraft for the launch vehicle ejection”, Keldysh Institute preprints, 2005, 038 |
| 6. |
Yu. G. Sikharulidze, V. A. Cherkashin, A. S. Karpov, R. K. Ivanov, “Determination of the save distance between the carrier aircraft and launch vehicle at switch-on of the first-stage engine in air launch”, Mat. Model., 17:11 (2005), 25–42  |
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