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Clarify Documentation of THR_MDL_FAC
The documentation of the thrust model parameter `THR_MDL_FAC` did not mention both thrust and "PWM" being relative values. Also the use of the term PWM could be misleading, since the model is applicable to CAN ESCs as well. This commit rephrases the user documentation string and a few source code comments, but no logic changes are made. Closes PX4/Firmware#13105
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@@ -235,7 +235,7 @@ enum { /* DSM bind states */
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#define PX4IO_P_SETUP_MOTOR_SLEW_MAX 24 /**< max motor slew rate */
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#define PX4IO_P_SETUP_THR_MDL_FAC 25 /**< factor for modelling static pwm output to thrust relationship */
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#define PX4IO_P_SETUP_THR_MDL_FAC 25 /**< factor for modelling motor control signal output to static thrust relationship */
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#define PX4IO_P_SETUP_THERMAL 26 /**< thermal management */
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