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| Rev | Author | Line No. | Line |
|---|---|---|---|
| 1775 | - | 1 | /* |
| 1612 | dongfang | 2 | #ifndef _ADXRS610_H |
| 3 | #define _ADXRS610_H |
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| 4 | |||
| 5 | #include "sensors.h" |
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| 1646 | - | 6 | |
| 1775 | - | 7 | / * |
| 1612 | dongfang | 8 | * Configuration for the ADXR610 gyros, as they are oriented and wired on the FC 2.0 ME board. |
| 1775 | - | 9 | * / |
| 1612 | dongfang | 10 | |
| 11 | #define GYRO_HW_NAME "ADXR" |
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| 12 | #define GYRO_HW_FACTOR 1.2288f |
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| 13 | |||
| 1775 | - | 14 | / * |
| 1612 | dongfang | 15 | * Correction factor - determined experimentally: Hold the copter in the hand, and turn it 90 degrees. |
| 16 | * If AnglePitch or AngleRoll in debug in MK-Tool changes by x degrees, multiply the value here by x/90. |
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| 17 | * If the hardware related contants are set correctly, flight should be OK without bothering to |
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| 18 | * make any adjustments here. It is only for luxury. |
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| 1775 | - | 19 | * / |
| 1612 | dongfang | 20 | #define GYRO_PITCHROLL_CORRECTION 1.0f |
| 21 | |||
| 1775 | - | 22 | / * |
| 1612 | dongfang | 23 | * Same for yaw. |
| 1775 | - | 24 | * / |
| 1612 | dongfang | 25 | #define GYRO_YAW_CORRECTION 1.0f |
| 26 | |||
| 27 | #endif |
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| 1775 | - | 28 | */ |