Faster speed. Shorter endurance. Increased maneuverability.
UAV Loading and Performance
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the rudder. the ailerons. the stabilizer.
increase if the CG is moved forward. remain the same regardless of gross weight. change with an increase in gross weight.
have a tendency to spin. be more difficult to control. stall at a higher airspeed.
the stabilizer. the ailerons. the rudder.
airplane’s center line and the relative wind. chord line of the wing and the relative wind. airplane’s longitudinal axis and that of the air striking the airfoil.
34 pounds. 38 pounds. 47 pounds.
Attack. Dihedral. Incidence.
Remote Pilot in Command Manufacturer. Owner or operator
the CG is shifted rearward to the aft CG limit. the gross weight is reduced. the airplane is subjected to maneuvers other than straight and level flight.