A remote pilot attaches an aftermarket payload to their UAS, causing the Centre of Gravity (CG) to shift significantly behind the manufacturer's recommended aft limit. What is the most likely flight characteristic they will experience?
-
A
Increased longitudinal stability and sluggish pitch control.
-
B
A tendency for the UAS to pitch up and reduced longitudinal stability.
-
C
Improved forward flight speed due to better aerodynamics.
-
D
No noticeable change, as the flight controller will compensate.