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| Rev | Author | Line No. | Line |
|---|---|---|---|
| 1775 | - | 1 | /* |
| 1612 | dongfang | 2 | #ifndef _ENC03_FC13_H |
| 3 | #define _ENC03_FC13_H |
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| 4 | |||
| 5 | #include "sensors.h" |
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| 1775 | - | 6 | / * |
| 1612 | dongfang | 7 | * Configuration for the ENC-03 gyros and oriented and wired on FC 1.3 (with DAC). |
| 1775 | - | 8 | * / |
| 1612 | dongfang | 9 | |
| 10 | #define GYRO_HW_NAME "ENC" |
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| 11 | #define GYRO_HW_FACTOR 1.304f |
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| 12 | |||
| 1775 | - | 13 | / * |
| 1612 | dongfang | 14 | * Correction factor - determined experimentally: Hold the copter in the hand, and turn it 90 degrees. |
| 15 | * If AnglePitch or AngleRoll in debug in MK-Tool changes by x degrees, multiply the value here by x/90. |
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| 16 | * If the hardware related contants are set correctly, flight should be OK without bothering to |
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| 17 | * make any adjustments here. It is only for luxury. |
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| 1775 | - | 18 | * / |
| 1612 | dongfang | 19 | #define GYRO_PITCHROLL_CORRECTION 1.11f |
| 20 | |||
| 1775 | - | 21 | / * |
| 1612 | dongfang | 22 | * Same for yaw. |
| 1775 | - | 23 | * / |
| 1612 | dongfang | 24 | #define GYRO_YAW_CORRECTION 1.28f |
| 25 | #endif |
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| 1775 | - | 26 | */ |