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config.h [2016/11/19 08:45] silverxxx |
config.h [2017/11/09 22:08] (current) sirdomsen |
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| * Settings that affect flight control, such as rate , expo, and switch assignment | * Settings that affect flight control, such as rate , expo, and switch assignment | ||
| - | * Settings | + | * Settings |
| - | * settings | + | * settings |
| This info is for the H8 mini code, some settings may differ slightly in some builds. | This info is for the H8 mini code, some settings may differ slightly in some builds. | ||
| Line 19: | Line 19: | ||
| === Rate === | === Rate === | ||
| - | The rate is changed by the following lines in control.h file. The unit is degrees / second, and is for low rates. So on low rates (stock tx) the quad will perform a 180 degree turn in 1 second at maximum control deflection. | + | The rate is changed by the following lines in config.h file. The unit is degrees / second, and (on some firmwares) |
| < | < | ||
| Line 35: | Line 35: | ||
| #define HIRATEMULTI 2.0f | #define HIRATEMULTI 2.0f | ||
| #define HIRATEMULTIYAW 2.0f | #define HIRATEMULTIYAW 2.0f | ||
| + | </ | ||
| + | |||
| + | **Note**: On some firmwares the **high** | ||
| + | |||
| + | < | ||
| + | // rate in deg/sec | ||
| + | // for acro mode | ||
| + | #define MAX_RATE 360.0 | ||
| + | #define MAX_RATEYAW 360.0 | ||
| + | |||
| + | #define LOW_RATES_MULTI 0.5f | ||
| </ | </ | ||
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| CHANNEL10, | CHANNEL10, | ||
| CHANNEL11, | CHANNEL11, | ||
| + | CHANNEL12, | ||
| </ | </ | ||
| - | <font 14px/ | + | Silverware also supports to set simply a channel number as numbered in DeviationTX: |
| <font 14px/ | <font 14px/ | ||
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| The auto throttle will keep a constant upwards thrust as the quad leans in one direction. Used in level mode, usually. | The auto throttle will keep a constant upwards thrust as the quad leans in one direction. Used in level mode, usually. | ||
| - | Example: Suppose the quadcopter is at a 45 degrees angle. Because of the angle, only half the thrust will contribute to maintaining | + | Example: Suppose the quadcopter is at a 45 degrees angle. Because of the angle, only half the thrust will contribute to maintaining |
| < | < | ||