I have to try and place it into non linear State-Space form first if that is possible. We have a new control Algorithm so we are taken on a Quad-rotor UAV as a case study.
I have uploaded the dynamics equations to flickr.... If you could cast an eye over it and give your opinion it would be great:
http://www.flickr.com/photos/spitsplat/
For the control Algorithm to work we require 6 inputs and 6 outputs from a MIMO State-Space model of the UAV Dynamics. For 6 inputs, and for an academic exercise, we have decided to make the rotors pitchable (opposed rotors coupled).
So the inputs become (S1-S3), (S2-S4),(S1+S3), (S2+S4), Alpha and Beta.
Any help would be great.... Hopefully we’ll get the thing of the ground and I’ll post the video’s on youtube.