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fixes to INS backported from portugal flight branch
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@ -659,9 +659,9 @@ static int32_t updateAttitudeINSGPS(bool first_run, bool outdoor_mode)
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dT = PIOS_DELAY_DiffuS(ins_last_time) / 1.0e6f;
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dT = PIOS_DELAY_DiffuS(ins_last_time) / 1.0e6f;
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GyrosBiasGet(&gyrosBias);
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GyrosBiasGet(&gyrosBias);
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float gyros[3] = {(gyrosData.x + gyrosBias.x) * F_PI / 180.0f,
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float gyros[3] = {(gyrosData.x - gyrosBias.x) * F_PI / 180.0f,
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(gyrosData.y + gyrosBias.y) * F_PI / 180.0f,
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(gyrosData.y - gyrosBias.y) * F_PI / 180.0f,
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(gyrosData.z + gyrosBias.z) * F_PI / 180.0f};
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(gyrosData.z - gyrosBias.z) * F_PI / 180.0f};
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INSStatePrediction(gyros, &accelsData.x, dT);
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INSStatePrediction(gyros, &accelsData.x, dT);
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AttitudeActualData attitude;
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AttitudeActualData attitude;
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@ -797,7 +797,7 @@ static int32_t updateAttitudeINSGPS(bool first_run, bool outdoor_mode)
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velocityActual.Down = Nav.Vel[2];
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velocityActual.Down = Nav.Vel[2];
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VelocityActualSet(&velocityActual);
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VelocityActualSet(&velocityActual);
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if(fabs(Nav.gyro_bias[0]) > 0.1f || fabs(Nav.gyro_bias[1]) > 0.1f || fabs(Nav.gyro_bias[2]) > 0.1f) {
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if(fabs(Nav.gyro_bias[0]) > 0.5f || fabs(Nav.gyro_bias[1]) > 0.5f || fabs(Nav.gyro_bias[2]) > 0.5f) {
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float zeros[3] = {0.0f,0.0f,0.0f};
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float zeros[3] = {0.0f,0.0f,0.0f};
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INSSetGyroBias(zeros);
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INSSetGyroBias(zeros);
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}
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}
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