Name
|
Description
|
ANoise
|
Measurement noise value for the A component
|
DataSpanDuration
|
Duration of the data span over which to generate observations. Note that the final observation may fall prior to the end of the data span if the propagation model doesn't generate a state at that time.
|
DataSpanStartEpoch
|
The epoch for the start of the observation span to be generated.
|
DeclaredName
|
The name of the object as declared.
|
ElementSetToUse
|
A flag indicating the element set to use when estimating the orbit state.
|
HNoise
|
Measurement noise value for the H component
|
KNoise
|
Measurement noise value for the K component
|
LongitudeNoise
|
Measurement noise value for the Longitude component
|
Name
|
The name displayed for this object in output windows such as views, plots, and reports.
|
ObjectBeingObserved
|
The Spacecraft object to be fit to the reference trajectory.
|
ObjectId
|
The unique identifier for the object.
|
ObjectType
|
The type of the object.
|
PNoise
|
Measurement noise value for the P component
|
QNoise
|
Measurement noise value for the Q component
|
ReferenceSpacecraft
|
The Spacecraft object whose propagation model defines the reference trajectory.
|
SpanIntervalOption
|
The option for specifying the observation interval.
|
SpanStartEpochOption
|
The option for specifying the initial observation epoch.
|
StepSize
|
The number of seconds between each generated observation.
|
VXNoise
|
Measurement noise value for the VX component
|
VYNoise
|
Measurement noise value for the VY component
|
VZNoise
|
Measurement noise value for the VZ component
|
XNoise
|
Measurement noise value for the X component
|
YNoise
|
Measurement noise value for the Y component
|
ZNoise
|
Measurement noise value for the Z component
|