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Chinese Journal of Mechanical Engineering

Table 3 Optimal solutions

From: Optimal Design and Force Control of a Nine-Cable-Driven Parallel Mechanism for Lunar Takeoff Simulation

 

Angle θ1 (°)

Angle θ2 (°)

Angle θ3 (°)

Radius R1 (m)

Radius R2 (m)

SUM_DWS

1

3.25

6.62

57.56

0.26

0.05

8559.6

2

4.73

3.61

77.06

0.25

0.11

7478.7

3

5.85

6.17

62.59

0.23

0.08

7343.9

4

4.82

8.03

53.24

0.28

0.11

7554

5

2.69

4.76

54.77

0.29

0.11

8065.4

6

5

5

60

0.25

0.1

6551

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