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This standard addresses spacecraft utilizing continuous low-thrust propulsion systems and,
considering the particularities of their attitude and orbit control operations, defines the
classification of executable in-orbit tasks. It specifies the associated operational modes, control
strategies, critical mission phases, and operational requirements for each task type, with a
particular focus on coordination between onboard autonomy and ground segment support.
Additionally, this standard identifies the specific constraints and supplementary requirements
applicable to the use of continuous low-thrust propulsion as an operational means for attitude
and orbit control.
This standard is primarily applicable to spacecraft employing continuous low-thrust propulsion
technologies—such as electric propulsion—for performing in-orbit attitude and orbit control
operations
Reģistrācijas numurs (WIID)
95039
Darbības sfēra
This standard addresses spacecraft utilizing continuous low-thrust propulsion systems and,
considering the particularities of their attitude and orbit control operations, defines the
classification of executable in-orbit tasks. It specifies the associated operational modes, control
strategies, critical mission phases, and operational requirements for each task type, with a
particular focus on coordination between onboard autonomy and ground segment support.
Additionally, this standard identifies the specific constraints and supplementary requirements
applicable to the use of continuous low-thrust propulsion as an operational means for attitude
and orbit control.
This standard is primarily applicable to spacecraft employing continuous low-thrust propulsion
technologies—such as electric propulsion—for performing in-orbit attitude and orbit control
operations
