Yes we did it !!!
The pitch of the aircraft has been determined by fusing the pitch rate gyro and x accelero.
Well it was not that easy, it took us some time to understand the basic idea of Kalman, then we made our own program of Kalman (which was a disaster) and finally some wonderful work done by Tramell Hudson of Rotomotion inc came to our rescue.
Thank you Mr. Hudson
watch this space for more exciting news
Next Target: EKF (Extended Kalman Filter) to compute roll of the aircraft.
Chak and Joseph
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