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. |
![]() | Stop immediately if propagation begins beyond an active epoch stopping condition. |
![]() | Gets or sets the time interval between calculated ephemeris output points. Uses Time Dimension. |
![]() | Get the stopping conditions defined for the segment. |
Implemented Interface |
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IAgVAMCSSegment |
IAgComponentInfo |
IAgCloneable |
Name |
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AgVAMCSHold |