Orbit maneuver exhibits significant applications in formation flight, spacecraft information supporting and on-orbit servicing etc. In the paper, we pay more attention to analyze spacecraft's control domain under extra maneuver ability. According to emulate different direction velocity increment in different plane thrown to spacecraft, we analyze the variation of orbit parameters change with velocity increment. Furthermore, we give some conclusions which can provide theory foundation for the task of spacecraft information supporting and on-orbit servicing.
Emulation and analysis of spacecraft control domain
2014-08-01
268768 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Emulation of embedded spacecraft computers
AIAA | 1977
|Emulation of embedded spacecraft computer
Tema Archiv | 1977
|