I am trying to use the lightweight airplane design example on simulink now, but I cannot link the FlightGear to Simulink, do you know what happen? Also, is it this model available online, please?
because using unit quaternion parameters have no singularity as euler angles do for example pitch up 90 degrees. Fly a loop and watch what happens to the roll angle.
Hey, Can you tell me how to add other variant subsystem in existing model when already a subsystem is working. I want to change Simulink 3D visualization to FlightGear visualization in my block diagram under visualization subsystem.
I do not thrust an autopilot designed by an control systems engineer who has no piloting experience and is not aware of possible failures and limits. Look for example at the case of of the vertical speed control mode used near the aircraft's service altitude, when it cannot recognize an imminent stall. 2 pilots on a repositioning flight paid the ultimate price using that mode at 41000 ft. Who designed the MCAS system for the B 757 Max? A control system engineer which is also a rated pilot would never had the pitch system enter repeated trim inputs to force the nose down in response to a single AoA sensor without cross checking what the actual attitude and CAS of the aircraft is , information available from dual computers. Worse is the total absence of a 'failure modes and effects analysis' before such a system is implemented on a real airplane.
After running the main function from the file exchange, Error using fgets Invalid file identifier. Use fopen to generate a valid file identifier. Error in fgetl (line 33) [tline,lt] = fgets(fid); Error in drawDATCOMaircraft (line 35) tempstr=fgetl(tempdat);
