stabilization_plane_pid
Basic fixed-wing PID controller for rotorcraft firmware using float euler implementation
STABILIZATION_PLANE_ |
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|---|---|---|
Name |
Value |
Description |
SP_MAX_PHI |
45. |
max setpoint for roll angle |
SP_MAX_THETA |
45. |
max setpoint for pitch angle |
PHI_PGAIN |
400 |
feedback roll P gain |
PHI_DGAIN |
300 |
feedback roll D gain |
PHI_IGAIN |
100 |
feedback roll I gain |
THETA_PGAIN |
400 |
feedback pitch P gain |
THETA_DGAIN |
300 |
feedback pitch D gain |
THETA_IGAIN |
100 |
feedback pitch I gain |
Depends
- stabilization_rotorcraft
- @attitude_command
Provides
- commands