parameter | explanation |
---|---|
roll_rate | Maximum roll rate limit for your ariplane. Must not exceed physical limit of your plane |
pitch_rate | Maximum pitch rate limit for your ariplane. Must not exceed physical limit of your plane |
yaw_rate | Maximum yaw rate limit for your ariplane. Must not exceed physical limit of your plane |
fw_p_level | Self-leveling strength. Bigger value means sharper response |
fw_i_level | Self-leveling filtering. Usual value for airplanes is 1-5 Hz |
max_angle_inclination_rll | Maximum roll angle in [0.1 deg] units |
max_angle_inclination_pit | Maximum pitch angle in [0.1 deg] units |
tpa_breakpoint | Cruise throttle (expected throttle that you would be flying most of the time) |
tpa_rate | Amount of TPS curve to apply (usually should be in range 50-80 for most airplanes) |
roll_rate
and pitch_rate
values). Small and agile flying wings can reach 180-200 deg/s.