Description

Public Methods

AddAcceleration	Add the acceleration in meters/second^2 in the given frame to the force model.
AddDerivativeOutputValue	Sets the value of a first derivative in internal units.
DateElements	Current epoch in requested time scale expressed in date format. Year [yyyy], DayOfYear [1-366], Month [1-12], DayOfMonth [1-31], Hour [0-23], Minute [0-59], Seconds [0-60].
DateElements_Array	Current epoch in requested time scale expressed in date format returned as the array: Year [yyyy], DayOfYear [1-366], Month [1-12], DayOfMonth [1-31], Hour [0-23], Minute [0-59], Seconds [0-60]. Useful for scripting clients.
DateString	Current epoch expressed using the date format abbreviation specified.
DayCount	Current epoch in requested time scale expressed in day count format.
DayCount_Array	Current epoch in requested time scale expressed in day count format returned as an array representing wholeDays, secsIntoDay. Useful for scripting clients.
GetInputValue	Gets the value of an input to the plugin in internal units.
IndicateEvent	Marks an event to the propagator.
PosVel	Current position (meters) and velocity (meters/second) in the requested frame.
PosVel_Array	Current position (meters) and velocity (meters/second) in the requested frame returned as an array representing x, y, z, vx, vy, vz. Useful for scripting clients.
RefEpochElements	Reference epoch expressed in requested time scale in day count and date formats. WholeDays, SecsIntoDay, Year [yyyy], DayOfYear [1-366], Month [1-12], DayOfMonth [1-31], Hour [0-23], Minute [0-59], Seconds [0-60].
RefEpochElements_Array	Reference epoch expressed in requested time scale in day count and date formats as the array: WholeDays, SecsIntoDay, Year [yyyy], DayOfYear [1-366], Month [1-12], DayOfMonth [1-31], Hour [0-23], Minute [0-59], Seconds [0-60]. Useful for scripting clients.
RefEpochString	Reference epoch expressed using the date format abbreviation specified.
SetMaxStep	Sets the maximum step size in seconds for the propagator.
SetParameterOutputValue	Sets the value of a parameter output of the plugin in internal units.
StopPropagation	Stops propagation. For fatal errors.
TransformVector	Transforms a vector from the input frame to the output frame.
TransformVector_Array	Transforms a vector from the input frame to the output frame (in internal units) returned as an array representing x, y, z. Useful for scripting clients.

Public Properties

CbName	Name of the central body used as reference frame origin.
Mu	Gravitational constant in meters^3/second^2.
TimeSinceRefEpoch	Current epoch expressed in seconds since reference epoch.

CoClasses that Implement IAgAsEOMFuncPluginStateVector