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.
^ Name ^ Min ^ Max ^ Default ^ Multiplier ^ Enabled ^ Comment ^
| BAT_V_EMPTY | 0.9 | 100.0 | 3.2 | 1 | 1 | Voltage of an empty battery cell |
| BAT_V_FULL | 1.0 | 200.0 | 4.05 | 1 | 1 | Voltage of a full battery cell |
| BAT_N_CELLS | 1 | 100 | 3 | 1 | 1 | Number of SERIAL battery cells. Typically this ranges from 2S to 6S in small-scale UAVs |
| BAT_V_SCALING | 0.001 | 1.0 | 0.00838 | 1 | 1 | Conversion from ADC ticks to battery voltage. Depends on the connected board, calibrate with a multimeter. |
| MC_ATTRATE_P | 0.0 | 20.0 | 0.20 | 1 | 1 | Multirotor attitude rate control P gain. This gain controls how much of the motor thrust should be used to control angular velocity. A larger number will increase the control response, but will make the system also more twitchy. |
| MC_ATTRATE_D | 0.0 | 20.0 | 0.05 | 1 | 1 | Multirotor attitude rate control D gain. A large value will allow to damp oscillations due to a high P gain, but will make the system response suspectible to noise.|
| MC_ATT_P | 0.0 | 20.0 | 0.20 | 1 | 1 | Multirotor attitude control proportional (P) gain. This defines how strong the response of the system will be to an attitude error|
| MC_ATT_D | 0.0 | 20.0 | 0.05 | 1 | 1 | Multirotor attitude control D gain. A large value will allow to damp oscillations due to a high P gain, but will make the system response suspectible to noise.|
| FW_ROLLRATE_P | 0.0 | 20.0 | 0.30 | 1 | 1 | Fixed wing roll rate control P gain. This gain controls how strong the ailerons or rudder should be actuated in order to achieve a certain roll rate. A larger number will increase the control response, but will make the system also more twitchy. |
| FW_HEADING_P | 0.0 | 20.0 | 4.00 | 1 | 1 | Fixed wing heading error to bank angle gain |
