Hi all,
I'm working on creating a Simulink simulation model for an unpowered projectile-shape-like air glider using the Aerosim Blockset . The glider has a wing kit and a set of 4 X-form control fins. I want to calculate the aerodynamic coefficients including stability and control derivatives to fill up the aerodynamic model block in the Aerosim Blockset. Any recommendation what software tools can I use to do this job?
I already worked with DATCOM. But the results I got failed to verify the linearized model.
I would appreciate your help!
Thanks
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