Optical Properties

The OpticalProperties attribute applies to a satellite-based tracking instrument or facility object. In the case of a satellite-based tracking instrument, ODTK applies optical properties to space-based tracking where one satellite produces measurements of another satellite. OpticalProperties consists of the attributes below.

Target must be lit

Select true or false. If true, optical measurements, right ascension, and declination are only valid if the target satellite is illuminated by the Sun. The simulator does not generate such measurements, and the filter does not process them.

Space background required

Select true or false. If true, ODTK considers optical measurements, right ascension, and declination invalid if the line of sight from the tracking satellite to target satellite comes closer to the Earth than allowed by the MinGrazingAlt setting on the TrackingInstrument. The simulator does not generate such measurements, and the filter does not process them.

Polar exclusion

Enter an angle value for the PolarExclusion attribute. ODTK considers optical measurements, right ascension, and declination invalid if they are within the exclusion angle of either the north or south inertial poles. The simulator does not generate such measurements, and the filter does not process them.

Max sun elevation

Enter an angle value for the MaxSunElevation attribute. ODTK considers optical measurements, right ascension, and declination invalid if the elevation angle of the sun relative to the Facility is greater than the entered value. The simulator does not generate such measurements, and the filter does not process them.

Min sun exclusion

Enter an angle value for the MinSunExclusion attribute. ODTK considers optical measurements, right ascension, and declination invalid if the angle between the line of sight from the tracker to the satellite and direction of the sun relative to the tracker is less than the entered value. The simulator does not generate such measurements, and the filter does not process them.

Min moon exclusion

Enter an angle value for the MinMoonExclusion attribute. ODTK considers optical measurements, right ascension, and declination invalid if the angle between the line of sight from the tracker to the satellite and direction of the moon relative to the tracker is less than the entered value. The simulator does not generate such measurements, and the filter does not process them. This setting applies only for Earth-based trackers.

Min Earth exclusion

Enter an angle value for the MinEarthExclusion attribute. ODTK considers optical measurements, right ascension, and declination invalid if the angle between the line-of-sight from the tracker to the satellite and direction of the Earth relative to the tracker is less than the entered value. The simulator does not generate such measurements, and the filter does not process them. This setting only applies for Moon-based trackers.

Max solar phase angle

Enter an angle value for the MaxSolarPhaseAngle attribute. ODTK considers optical measurements, right ascension, and declination invalid if the calculated solar phase angle, measured as the angle between vector from the target satellite to the observer and the vector from the target satellite to the sun, is less than the constraint value. The simulator does not generate such measurements, and the filter does not process them.

 

Optical navigation camera

The OpNavCamera attribute applies to a satellite-based tracking instrument. For details on this attribute, see the Optical Navigation Camera help page.

Reference frame

Use the ReferenceFrame attribute to specify the reference frame of the right ascension and declination angles. ODTK uses this reference frame in the creation of simulated data and in the processing of data if the tracking data file does not explicitly specify the reference frame for the observations. Facilities located on bodies other than the Earth are limited to the selections of ICRF and MEME J2000.

Reference Frames
Frame Description
ICRF International Celestial Reference Frame
MEME B1950 The mean equator and mean equinox of B1950 reference frame, based on FK4
MEME J2000 The mean equator and mean equinox of J2000 reference frame, based on FK5
MEME Of Date (mean of date) Defined by the mean equator and mean equinox of the observation epoch, based on FK5
MEME Of Jan 0 Defined by the mean equator and mean equinox of January 0 of the year of the observation, based on FK5
MEME Of UTC 00:00 Defined by the mean equator and mean equinox at zero hours on the UTC day of the observation epoch, based on FK5
TEME Of Date Defined by the true equator and mean equinox of the observation epoch, based on FK5
TEME Of Jan0 Defined by the true equator and mean equinox of January 0 of the year of the observation, based on FK5
TEME Of UTC 00:00 Defined by the true equator and mean equinox at zero hours on the UTC day of the observation epoch, based on FK5
TETE Of Date (true of date) Defined by the true equator and true equinox of the observation epoch, based on FK5
TETE Of Jan0 Defined by the true equator and true equinox of January 0 of the year of the observation, based on FK5
TETE Of UTC 00:00 Defined by the true equator and true equinox at zero hours on the UTC day of the observation epoch, based on FK5

Aberration corrections

Use the AberrationCorrections attribute to enter corrections for ODTK to apply in the processing of optical measurements. ODTK also applies aberration corrections to azimuth and elevation measurements when the LightTimeDelay setting on the corresponding measurement statistics entry is set to true.

Aberration Correction Options
Option Description
All Tells ODTK to correct observations for annual and diurnal aberration
Annual Tells ODTK to correct observations for annual aberration, assuming that diurnal aberration has been removed
Diurnal Tells ODTK to correct observations for diurnal aberration, assuming that annual aberration has been removed
None Specifies that observations have been previously corrected for all aberration effects

These settings may also be interpreted as the aberration effects to be added to measurements during simulation.