mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-07-17 06:10:35 +08:00
mc_att_control_params: lower default roll and pitch attitude gains from 6.5 to 4
6.5 is a relatively high value that was used mostly on smaller, low inertia vehicles ~250-500mm diagonal. There it works great but on larger, higher intertia vehicles this leads to problems.
This commit is contained in:
@@ -50,7 +50,7 @@
|
||||
* @increment 0.1
|
||||
* @group Multicopter Attitude Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(MC_ROLL_P, 6.5f);
|
||||
PARAM_DEFINE_FLOAT(MC_ROLL_P, 4.0f);
|
||||
|
||||
/**
|
||||
* Pitch P gain
|
||||
@@ -63,7 +63,7 @@ PARAM_DEFINE_FLOAT(MC_ROLL_P, 6.5f);
|
||||
* @increment 0.1
|
||||
* @group Multicopter Attitude Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(MC_PITCH_P, 6.5f);
|
||||
PARAM_DEFINE_FLOAT(MC_PITCH_P, 4.0f);
|
||||
|
||||
/**
|
||||
* Yaw P gain
|
||||
|
||||
Reference in New Issue
Block a user