Voir la notice de l'article provenant de la source Math-Net.Ru
[1] Lure A.I., Analiticheskaya mekhanika, Fizmatgiz, M., 1961 | MR
[2] Beletskii V.V., Dvizhenie iskusstvennogo sputnika otnositelno tsentra mass, Nauka, M., 1965
[3] Filippov A.P., Kolebaniya deformiruemykh sistem, Mashinostroenie, M., 1970
[4] Morozov V.M., Ilinskaya A.V., “Ob ustoichivosti otnositelnogo ravnovesiya na krugovoi orbite dvukh tverdykh tel, soedinennykh massivnym uprugim sterzhnem”, Tr. X Mezhdunar. Chetaevskoi konf. “Analiticheskaya mekhanika, ustoichivost i upravlenie”, posvyaschennoi 110-letiyu N.G. Chetaeva (Kazan, 2012), v. 2, 383–392 | MR
[5] Sanyal A.K., Shen J., McClamroch N.H., “Dynamics and Control of an Elastic Dumbbell Spacecraft in a Central Gravitational Field”, Proc. 47th IEEE Conference on Decision and Control, Department of Aerospace Engineering, University of Michigan, Ann Arbor, 2003, 2798–2803
[6] Rumyantsev V.V., “O dvizhenii i ustoichivosti uprugogo tela s polostyu, soderzhaschei zhidkost”, Prikl. matem. i mekhan., 33:6 (1969), 946–957 | Zbl
[7] Morozov V.M., Rubanovskii V.N., Rumyantsev V.V., Samsonov V.A., “O bifurkatsii i ustoichivosti ustanovivshikhsya dvizhenii slozhnykh mekhanicheskikh sistem”, Prikl. matem. i mekhan., 37:3 (1973), 387–399 | Zbl
[8] Samsonov V.A., “O zadache minimuma funktsionala pri issledovanii ustoichivosti dvizheniya tela s zhidkim napolneniem”, Prikl. matem. i mekhan., 31:3 (1967), 523–526 | Zbl