Javacat1
Member
I'm working as part of my university's Spaceport team to develop a SRAD flight computer to assist with experiment control and future use with an airbrakes system for hybrid motors. We're looking to use a mix of baro + accel + GPS for state derivation, and one of the key points is trying to determine vertical orientation for using the accelerometer as part of a kalman filter to determine altitude (among also being able to determine attitude).
I've read the Madgwick paper Here and also found these two threads: (1, 2) with information, but I'm struggling with making sure we're actually getting proper dynamics information out. Do y'all have any suggestions/places to look that may help?
I've read the Madgwick paper Here and also found these two threads: (1, 2) with information, but I'm struggling with making sure we're actually getting proper dynamics information out. Do y'all have any suggestions/places to look that may help?