stabilization_attitude_fw
Legacy attitude and lateral (heading) control for fixedwing aircraft
H_CTL_ |
||
|---|---|---|
Name |
Value |
Description |
COURSE_PGAIN |
1.0 |
feedback heading P gain |
COURSE_DGAIN |
0.3 |
feedback heading D gain |
ROLL_MAX_SETPOINT |
45. |
max roll setpoint |
PITCH_MAX_SETPOINT |
30. |
max pitch up setpoint |
PITCH_MIN_SETPOINT |
-30. |
max pitch down setpoint |
PITCH_PGAIN |
12000. |
feedback pitch P gain |
PITCH_DGAIN |
1.5 |
feedback pitch D gain |
ELEVATOR_OF_ROLL |
1250 |
feedforward pitch to roll coupling |
ROLL_SLEW |
0.1 |
roll slew rate limiter |
ROLL_ATTITUDE_GAIN |
7500 |
feedback roll P gain |
ROLL_RATE_GAIN |
1500 |
feedback roll rate P gain (roll D gain) |
Depends
- @attitude_command
Provides
- commands