FIELD: transport.
SUBSTANCE: invention relates to control over geostationary spacecraft during reservation and timely putting into operation. At passive spacecraft draft from starting position of reservation (SPR) to working orbital position (stay point) minimizes power consumption of spacecraft onboard systems. For this spacing between SPR and stay point is selected with due allowance for guaranteed term of vacant spacecraft and time for placing of spacecraft to SPR. Spacecraft is changed over to duty mode and, then, to hardware spin-up mode. Reservation terminated, spacecraft us removed from spin-up mode.
EFFECT: correction system working fluid saving, decelerated replacement of spacecraft.
1 dwg
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