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ROBOMECH Journal

Table 2 Model differences

From: Uniaxial attitude control of uncrewed aerial vehicle with thrust vectoring under model variations by deep reinforcement learning and domain randomization

Model

Weight, COG, Inertia

\(I_{yy}\)

m

\((x_G, z_G)\)

Model 1

–

-

–

Model 2

+6.1 \(\%\)

(+ 3.8, + 7.5) mm

+ 11\(\%\)

Model 3

+10 \(\%\)

(+ 6.4, + 13) mm

+ 20\(\%\)

Model 4

+15 \(\%\)

(+ 9.6, + 17) mm

+ 28\(\%\)

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