For control difference thrust is what is pertinent. How is differential thrust achieved with a single PID control? I am basically asking if the system is SISO of SIMO? I am recreating a controller in labview whereby a single is isolated…"
Ive been working on a similar concept but how are you compensation for in flight pitch? The role of the horizontal stabilizer is replace by the rapid movement of the tilt rotor mechanism? Compensation of the roll moments?