Zobrazeno 1 - 4
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pro vyhledávání: '"M. V. Palkin"'
Publikováno v:
Mekhatronika, Avtomatizatsiya, Upravlenie. 21:651-655
A task of a pair formation flying satellites optimal relative motion control is described. It is presented as a Lagrange problem of satellite relative motion by the criterion of the control acceleration minimization. The сontrol acceleration term co
Autor:
M. V. Palkin, I. P. Titkov
Publikováno v:
Mekhatronika, Avtomatizatsiya, Upravlenie. 20:308-313
A problem of a formation flying satellites maneuver control is presented. Among the most important criteria for satellite formation flying control system are active period maximization, precision of the configuration, secure motion (without collision
Autor:
M. V. Palkin
Publikováno v:
Mekhatronika, Avtomatizatsiya, Upravlenie. 20:52-58
A problem of a formation flying control is observed. As an example a concept of a multysatellite configuration ("space commercial") is described. Space advertisement is realized by groups of specialized free flying and cable-connected satellites, and
Autor:
M. V. Palkin
Publikováno v:
Nauka i Obrazovanie, Vol 0, Iss 8, Pp 100-115 (2015)
The term “formation flying” implies coordinated movement of at least two satellites on coplanar and non-coplanar orbits with a maximum distance between them being much less than the length of the orbit. Peculiarities of formation flying concept a