Properties for a Hold segment.
![]() |
Disables the specified control parameter. |
![]() |
Enables or disables the specified control parameter. |
![]() |
Sees if the specified control is enabled. |
![]() |
Returns whether or not the control parameters can be set. |
![]() |
Enable Hold Altitude - if true, the spacecraft's attitude is fixed within the hold frame. |
![]() |
Enable Maximum Propagation Time - if true, the maximum propagation time will be enforced. |
![]() |
If true, Astrogator will issue a warning message if propagation is stopped by the Maximum Propagation Time parameter. |
![]() |
Hold Frame - the reference frame of the Hold segment. |
![]() |
Maximum Propagation Time - the maximum propagation time, after which the segment will end regardless of whether the stopping conditions have been satisfied. Uses Time Dimension. |
![]() |
Minimum Propagation Time - the minimum time that must elapse from the beginning of the segment until Astrogator will begin checking stopping conditions for satisfaction. Uses Time Dimension. |
![]() |
Override Maximum Propagation Time - if there is a duration or epoch stopping condition that occurs after the maximum propagation time, ignore the maximum propagation time. |
![]() |
The time interval between calculated ephemeris output points. Uses Time Dimension. |
![]() |
The stopping conditions defined for the segment. |
Name |
---|
AgVAMCSHold |