implemented mapping between desired thrust and applied pwm in

multirotor mixer.

Signed-off-by: Roman <bapstroman@gmail.com>
This commit is contained in:
Roman
2016-12-15 23:39:53 +01:00
committed by Lorenz Meier
parent 22733b1501
commit d221313dfb
9 changed files with 95 additions and 3 deletions
+12
View File
@@ -3277,6 +3277,18 @@ PARAM_DEFINE_INT32(PWM_AUX_MAX, 2000);
*/
PARAM_DEFINE_INT32(PWM_AUX_DISARMED, 1500);
/**
* Thrust to PWM model parameter
*
* Parameter used to model the relationship between static thrust and motor
* input PWM. Model is: thrust = (1-factor)*PWM + factor * PWM^2
*
* @min 0.0
* @max 1.0
* @group PWM Outputs
*/
PARAM_DEFINE_FLOAT(THR_MDL_FAC, 0.65f);
/**
* Minimum motor rise time (slew rate limit).
*