Searched refs:SUN_E (Results 1 – 3 of 3) sorted by relevance
508 static final double SUN_E = 0.016713; // Eccentricity of orbit field in CalendarAstronomer604 norm2PI(trueAnomaly(meanAnomaly, SUN_E) + SUN_OMEGA_G), in getSunLongitude()
513 static final double SUN_E = 0.016713; // Eccentricity of orbit field in CalendarAstronomer609 norm2PI(trueAnomaly(meanAnomaly, SUN_E) + SUN_OMEGA_G), in getSunLongitude()
534 #define SUN_E 0.016713 // Eccentricity of orbit macro657 longitude = norm2PI(trueAnomaly(meanAnomaly, SUN_E) + SUN_OMEGA_G); in getSunLongitude()