Some Discussions about the Error Functions on SO(3) and SE(3) for the Guidance of a UAV Using the Screw Algebra Theory

Table 1

Data of the UAV in simulations.

Aerodynamic configuration	Flying-wing configuration	Mass of UAV	kg
Inertia; properties		Wing span of UAV	8.76 m
		Max thrust; (single engine of two)	500 kgf
		Max Mach	0.85
		Maximum flight altitude	15 km