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 * Growth of the integral per degree:
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 * Growth of the integral per degree:
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 * The hiResXXXX value per deg / s * INTEGRATION_FREQUENCY samples / sec * correction / a number divided by
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 * The hiResXXXX value per deg / s * INTEGRATION_FREQUENCY samples / sec * correction / a number divided by
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 * HIRES_GYRO_INTEGRATION_FACTOR (why???) before integration.
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 * HIRES_GYRO_INTEGRATION_FACTOR (why???) before integration.
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 * The value of this expression should be about 1250 (by setting HIRES_GYRO_INTEGRATION_FACTOR to something suitable).
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 * The value of this expression should be about 1250 (by setting HIRES_GYRO_INTEGRATION_FACTOR to something suitable).
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 */
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 */
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#define GYRO_DEG_FACTOR_PITCHROLL (int)(GYRO_RATE_FACTOR_PITCHROLL * INTEGRATION_FREQUENCY * GYRO_PITCHROLL_CORRECTION / HIRES_GYRO_INTEGRATION_FACTOR)
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#define GYRO_DEG_FACTOR_PITCHROLL (uint16_t)(GYRO_RATE_FACTOR_PITCHROLL * INTEGRATION_FREQUENCY * GYRO_PITCHROLL_CORRECTION / HIRES_GYRO_INTEGRATION_FACTOR)
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#define GYRO_DEG_FACTOR_YAW (int)(GYRO_RATE_FACTOR_YAW * INTEGRATION_FREQUENCY * GYRO_YAW_CORRECTION)
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#define GYRO_DEG_FACTOR_YAW (uint16_t)(GYRO_RATE_FACTOR_YAW * INTEGRATION_FREQUENCY * GYRO_YAW_CORRECTION)
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/*
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/*
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 * This is ([gyro integral value] / degree) / (degree / acc. sensor value) = gyro integral value / acc.sensor value
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 * This is ([gyro integral value] / degree) / (degree / acc. sensor value) = gyro integral value / acc.sensor value
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 * = the factor an acc. sensor should be multiplied by to get the gyro integral
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 * = the factor an acc. sensor should be multiplied by to get the gyro integral
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void updateCompass(void);
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void updateCompass(void);
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/*
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/*
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 * Dynamic gyro offsets. These are signed values that are subtracted from the gyro measurements,
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 * Dynamic gyro offsets. These are signed values that are subtracted from the gyro measurements,
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 * to help cancelling out drift and vibration noise effects. The dynamic offsets themselves
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 * to help canceling out drift and vibration noise effects. The dynamic offsets themselves
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 * can be updated in flight by different ways, for example:
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 * can be updated in flight by different ways, for example:
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 * - Just taking them from parameters, so the pilot can trim manually in a PC or mobile tool
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 * - Just taking them from parameters, so the pilot can trim manually in a PC or mobile tool
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 * - Summing up how much acc. meter correction was done to the gyro integrals over the last n
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 * - Summing up how much acc. meter correction was done to the gyro integrals over the last n