MAV_AUTOPILOT_PIXHAWK-MAV_TYPE_QUADROTOR.csv 382 Bytes
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EEPROM,variable name,Min,Max,Default,Multiplier,Enabled (0 = no, 1 = yes),Comment
HDNG2RLL_P, 0, 5, 0.7, 1, 1, NAV_ROLL_P - Navigation control gains. Tuning values for the navigation control PID loops. The P term is the primary tuning value. This determines how the control deflection varies in proportion to the required correction.
SYS_TYPE, 0, 15, 1, 1, 1, System type (airframe)