Name
|
Description
|
Clear
|
Removes all elements from the List.
|
ClearSavedStates
|
Clears previous saved states for this object.
|
GetFromFile
|
Load the object state from the specified FreeFlyer object file.
|
GetFromString
|
Load the object state from the specified string.
|
LoadRinexNavFile
|
Populates a Formation with one Spacecraft for each SatelliteId in the specified Rinex Navigation file and then initializes the Spacecraft with that state. This method also attaches a sensor to each Spacecraft in the Formation.
|
LoadSP3Ephemeris
|
Populates a Formation with one Spacecraft for each SatelliteId in the specified SP3 Precise Ephemeris file and then initializes the Spacecraft with that state. This method also attaches a Sensor and GPS Receiver to each Spacecraft in the Formation.
|
LoadTLE
|
Adds a Formation Spacecraft for each state in the specified TLE file and then initializes the Spacecraft with that state. If you are loading a Spacecraft state from a TLE, you should use a SGP4 propagator when running your Mission Plan.
|
MaxEpoch
|
Returns the maximum epoch contained within the Formation.
|
MinEpoch
|
Returns the minimum epoch contained within the Formation.
|
PutToFile
|
Convert the object state to FreeFlyer object xml and write to a file.
|
PutToString
|
Convert the object state to FreeFlyer object xml and return as a string.
|
ReferenceEquals
|
Returns 1 if the argument refers to the calling object and 0 otherwise.
|
RemoveAt
|
Remove the object at the specific index.
|
ResetMethodStates
|
Resets any method states associated with the calling object.
|
Restore
|
Restore an object's state from a previously saved state.
|
Save
|
Save the object's state so that it can be restored later.
|
SetRandomStates
|
Populates the Formation with states from a random Gaussian distribution described by the provided covariance matrix. The dimension and order of the covariance matrix is assumed to be consistent with the ProcessAction properties held in the first Spacecraft in the formation. The number of states generated is determined by the size of the provided Formation.
|
Step
|
Steps each Spacecraft in the Formation using the current propagator step size.
|
StepToEpoch
|
Steps each Spacecraft in the Formation to the specified epoch.
|