2019
DOI: 10.1088/1742-6596/1294/3/032034
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Reliability Allocation and Optimization for(ROSS) of a Spacecraft by using Genetic Algorithm

Abstract: This paper focuses on the reliability of Reduction Oxygen Supply System (ROSS) of a Spacecraft which was calculated as a complex system using probability theory. The reliability of this system was assigned to study the possible approaches of the allocation of reliability values based on the minimization of the total cost in this system. The original results was included: (i) a critical point is a fixed purpose of a appropriate application. (ii) Using the reduction oxygen supply sy… Show more

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Cited by 28 publications
(3 citation statements)
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“…The geometry optimization uses shape derivatives from differential geometry, which provide sensitivity of the cost and constraints to local perturbations in the manifold [6][7][8][9]. The shape derivatives are given by: Let M be an n-dimensional differentiable manifold representing the design space.…”
Section: Optimization Modelmentioning
confidence: 99%
“…The geometry optimization uses shape derivatives from differential geometry, which provide sensitivity of the cost and constraints to local perturbations in the manifold [6][7][8][9]. The shape derivatives are given by: Let M be an n-dimensional differentiable manifold representing the design space.…”
Section: Optimization Modelmentioning
confidence: 99%
“…Considering modelling or measurement uncertainties, statistics appear in various reliability analysis activities, such as sampling and DOEs. An accurate reliability estimation method considering various uncertainties from measurements to modelling can play a significant role in improving the design and performance of mechanical and structural systems [7][8][9]. An effective SRA can also help with the justification of design for different working conditions based on design and performance requirements [10,11].…”
Section: Introductionmentioning
confidence: 99%
“…One of the first researchers to take up the reduction oxygen supply system (ROSS) study of a spacecraft system for the first time by Aggarwal [1], and due to the importance of the topic in terms of engineering and science, light was re-shed by several researchers such as Hassan et al [2]- [9] where the researchers discussed the reliability of this system and the study of mean time to failure (MTTF) using the engineering properties of many reliability limits. Also Abed et al [10] discussed the issue of optimizing the reliability of this system has solved by using a genetic algorithm.…”
Section: Introductionmentioning
confidence: 99%