Mirror/betaflight
1
0
Fork 0
mirror of https://github.com/betaflight/betaflight.git synced 2025-07-16 04:45:24 +03:00
Code Issues Wiki Activity

Added checking angle of attack limiter valid work conditions

Browse source
This commit is contained in:
demvlad 2025-04-18 08:54:05 +03:00
parent ff5cf0673d
commit 048ccc0045
4 changed files with 65 additions and 37 deletions
Download patch file Download diff file Expand all files Collapse all files

2
src/main/flight/pid.c
View file

@ -280,7 +280,7 @@ void resetPidProfile(pidProfile_t *pidProfile)
.afcs_pitch_accel_i_gain = 250, // elevator speed for 1g Z accel difference in %/sec *10
.afcs_pitch_accel_max = 80, // maximal positive Z accel value *10
.afcs_pitch_accel_min = 60, // maximal negative Z accel value *10
.afcs_wing_load = 5600, // wing load (mass / WingArea) g/decimeter^2 * 100. The g/decimeter^2 units is more comfortable for perception, than kg/m^2, i think
.afcs_wing_load = 560, // wing load (mass / WingArea) g/decimeter^2 * 10. The g/decimeter^2 units is more comfortable for perception, than kg/m^2, i think
.afcs_air_density = 1225, // The current atmosphere air density [mg/m^3], the MSA 1225 g/m^3 value is default. TODO: Dynamical air density computing by using baro sensors data
.afcs_lift_c_limit = 12, // Limit aerodinamics lift force coefficient value *10
.afcs_aoa_limiter_gain = 250, // elevator speed for 0.1 lift force coef difference in %/sec *10