Hello Team,
I’m currently working on a UAV with a tandem wing configuration designed as a tail-sitter. I’d appreciate your input on a few design aspects.
The aircraft features twin motors mounted on the leading edge of the front wing, while the rear wing is positioned lower on the fuselage to aid in pitching stability. I’m in the process of determining the optimal center of gravity (CG) for stable vertical and forward flight.
Also, I’m considering how to define the control surfaces. Should all surfaces be configured as ailevons (combining roll and pitch control), or would it be more appropriate to designate ailerons on the front wing and elevators on the rear wing?
Looking forward to your thoughts and suggestions.
Best regards,
Paras