Searched refs:omega (Results 1 – 4 of 4) sorted by relevance
280 double omega = 2.0 * Math.PI * f_notch / f_s; in Biquad() local282 a[1] = -2.0f * alpha * (float)Math.cos(omega); in Biquad()284 b[1] = -2.0f * (float)Math.cos(omega); in Biquad()
68 optional double omega = 21; field
117 double argumentOfLatitudeRadians = trueAnomalyRadians + ephemerisProto.omega; in calculateSatellitePositionAndVelocity()
243 …gpsEphemerisProto.omega = ephemeris.getEphemW().getInteger().intValue() * NAVIGATION_W_SCALE_FACTO… in toSingleEphemeris()