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Table 2. Summary of Test Problem
problem
obj/D
Search Range
Constraints
Ineq.
Eq.
CONSTR
2/2
[0.1,1],[0,5]
2
0
[-20,20] D
SRN
2/2
2
0
[0,10],[0,10],[1,5]
[0,6],[1,5],[0,10]
OSY
2/6
6
0
Table 3. Mean and standard deviation of hypervolume metric values obtained by four
Algorithm for benchmark problems
Instance
Hypervolume
(Runs=30)
CONSTR
( ref [1,10] )
SRN
( ref [300,150] )
OSY
( ref [0,200] )
mean
std
mean
std
mean
std
MOEA/D-CDP-ID
3.95e-1
1.07e+5
1.15e+5
1.054e+1
6.66e+5
1.58e+5
MOEA/D-CDP
1.049e+1
5.49e-3
3.48e+5
3.01e+4
7.42e+4
2.21e+4
NSGAII-CDP-ID
1.050e+1
5.34e-3
9.00e+5
9.46e+4
1.35e+5
6.29e+4
NSGAII-CDP
1.051e+1
2.881e-3
6.98e+5
7.09e+4
7.82e+4
7.42e+3
4
Engineering Optimization Problem
4.1
Two-Stage Planetary Gear Transmission System Optimization Problems
The design problem of two-stage planetary gear transmission system is a ten-variable
and bi-objective constrained multiobjective optimization problem [8] [12]. The goal
of the design is to minimize volume and the maximize efficiency of the two-stage
planetary gear transmission system.
Fig. 3. Two-stage planetary gear transmission system
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