Description
Returns a numerical value representing the percentage-of-shadow the Spacecraft encounters in its orbit with respect to Earth's shadow. The calculation is based on percentage of shadow the Spacecraft encounters during penetration into the penumbral region. Once into the umbral region the percentage of shadow is 100%.
The three regions of the specified CelestialObject's shadow, the umbra, penumbra, and annular, are shown in the image below. This method returns 100% when the Spacecraft is in the umbral shadow region, and 0% when the Spacecraft is in direct sunlight.
The three regions of a celestial body's shadow.
FreeFlyer's percent shadow calculation calculates percentage-of-shadow based on the area of the solar disk that can be seen by the Spacecraft. The calculation is based on the following formulas:
|
Where:
|
= The percentage-of-shadow
= The apparent angular radius of the Sun, in radians
= The apparent angular radius of the Earth, in radians
= The apparent angular separation of the centers of both bodies, in radians
(1) Equation 3.92, Page 83 of Montenbruck, Oliver and Gill, Eberhard, Satellite Orbits: Models, Methods, and Applications, Springer-Verlag Berlin Heidelberg 2000, Corrected 4th printing 2012
(3) Equation 3.93, Page 83 of Montenbruck, Oliver and Gill, Eberhard, Satellite Orbits: Models, Methods, and Applications, Springer-Verlag Berlin Heidelberg 2000, Corrected 4th printing 2012
Timing Precision Mode
This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.
Attributes
Type: |
number |
Access: |
read |
Syntax
myVariable1 = mySpacecraft1.PercentEarthShadow; |
See also
Coverage and Contact Analysis Guide