Multi-objective optimization on the shock absorber design for the lunar probe using nondominated sorting genetic algorithm II
In this article, the design on the shock absorber of the lunar probe soft landing can be considered as a single- or multi-objective optimization problem. Here, the optimized objective parameters include the maximum toppling stability, defined as D min , and the minimum stroke of primary strut energy...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
SAGE Publishing
2017-07-01
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Series: | International Journal of Advanced Robotic Systems |
Online Access: | https://doi.org/10.1177/1729881417720467 |