Searched refs:SUN_E (Results 1 – 4 of 4) 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()
510 static final double SUN_E = 0.016713; // Eccentricity of orbit field in CalendarAstronomer606 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()
META-INF/ META-INF/MANIFEST.MF com/ com/ibm/ com/ ...