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
