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5ac0a3043b
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