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Table 3 Aows performance under different conditions

From: Toward mission-dependent long robotic arm enhancement: design method of flying watch attachment allocation based on thrust drivability

Object gravity (N)

End effector position (m)

\(\zeta\) (reduction rate)

\({D}_{all}\) (human experience)

\({D}_{all}\) (AOWS)

10

[11,2,0.8]

2.16%

0.719

0.947

15

[5,2,0.8]

64.35%

0.775

0.909

15

[8,2,0.8]

23.28%

0.791

0.928

15

[11,2,0.8]

37.43%

0.719

0.946

20

[11,2,0.8]

35.58%

0.719

0.946