As you probably guess, I have read dozens of papers and thesis to reach here
never thought it would be so difficult.
but when it reaches to actually make one of them work,,, that's the hard part. I want to know if anyone has reached here and how does he get passed this stage. let me get you more insights... I have PID on pitch and roll and PI on yaw rate. my IMU outputs are pitch, roll, pitch rate, roll rate, yaw rate, accel on x,accel on Y and accel on z. But these outputs have errors and as long as a stable flight is concerned even these small errors count.
pid coefficients are guessed... based on trial and error and quadrotor is "stable" (so called
) but when you let it loose, it just goes to where it wants.
BTW, thank you so much th_sak, Hope santa brings you sth nice too,
I'm sure your paper will help...
second BTW, where is my promised image?