Felix, i am sure that i changed the value and flashed.
Ok.Can you please provide as much information for debugging as possible?
- Which branch(es) did you do this test on?
- Can you please post your airframe config?
- Need to know if you are using adaptive control...
- Depending on which gains (ATTITUDE_GAIN or ROLL_PGAIN) you have defined in your airframe file, slightly different control loops are used.
Hopefully we can refactor the whole fixedwing control soon....
About Gautier modification ... its on dev branch ?
What Gautier modification do you mean? Gautier didn't change anything... just explained the current state.