Voir la notice de l'article provenant de la source Math-Net.Ru
[1] Manuilov Yu. S., Novikov E. A., Kravtsov A. N., “Sintez i issledovanie optimalnogo regulyatora uglovoi stabilizatsii kosmicheskogo apparata nablyudeniya nezhestkoi konstruktsii”, Aviakosmicheskoe priborostroenie, 2011, no. 1, 16–25
[2] Zlochevskii S. I., Kubyshkin E. P., “O stabilizatsii sputnika s gibkimi sterzhnyami. I”, Kosmicheskie issledovaniya, 27:5 (1989), 643–651
[3] Zlochevskii S. I., Kubyshkin E. P., “O stabilizatsii sputnika s gibkimi sterzhnyami. II”, Kosmicheskie issledovaniya, 29:6 (1991), 828–839
[4] Andreichenko D. K., Andreichenko K. P., “K teorii stabilizatsii sputnikov s uprugimi sterzhnyami”, Izv. RAN. TiSU, 2004, no. 6, 150–163 | MR | Zbl
[5] Andreichenko D. K., Andreichenko K. P., “K teorii kombinirovannykh dinamicheskikh sistem”, Izv. RAN. TiSU, 2000, no. 3, 54–69 | MR
[6] Andreichenko D. K., Andreichenko K. P., “Dinamicheskii analiz i vybor parametrov modeli giroskopicheskogo integratora lineinykh uskorenii s plavayuschei platformoi”, Izv. RAN. TiSU, 2008, no. 4, 76–89 | Zbl
[7] Andreichenko D. K., “Effektivnyi algoritm chislennogo obrascheniya integralnogo preobrazovaniya Laplasa”, Zhurn. vychisl. mat. i mat. fiz., 40:7 (2000), 1030–1044 | MR | Zbl