guidance_basic_fw
Legacy vertical control for fixedwing aircraft based on throttle (default) or pitch
V_CTL_ |
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---|---|---|
Name |
Value |
Description |
POWER_CTL_BAT_NOMINAL |
11.1 |
nominal battery level |
ALTITUDE_PGAIN |
0.03 |
altitude loop P gain |
ALTITUDE_MAX_CLIMB |
2. |
max climb rate |
AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE |
0.32 |
nominal throttle for cruise flight |
AUTO_THROTTLE_MIN_CRUISE_THROTTLE |
0.25 |
min cruise throttle |
AUTO_THROTTLE_MAX_CRUISE_THROTTLE |
0.65 |
max cruise throttle |
AUTO_THROTTLE_LOITER_TRIM |
1500 |
loiter trim |
AUTO_THROTTLE_DASH_TRIM |
-4000 |
dash trim |
AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT |
0.15 |
feedforward throttle gain |
AUTO_THROTTLE_PGAIN |
0.01 |
feedback throttle P gain |
AUTO_THROTTLE_IGAIN |
0.1 |
feedback throttle I gain |
AUTO_THROTTLE_PITCH_OF_VZ_PGAIN |
0.05 |
feedforward pitch gain |
THROTTLE_SLEW_LIMITER |
2 |
throttle slew rate limiter |
Depends
- @navigation
Provides
- guidance
- attitude_command