Redundancy allocation optimizing in the satellite attitude determination and control system based on the exact solution algorithm

The redundancy allocation problem is to find an optimal allocation of redundant components by considering the set of resources and cost constraints. In this research, the satellite attitude determination and control system is studied and its components is introduced, then the reliability of this sys...

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Vydáno v:	Communications in statistics. Theory and methods Ročník 53; číslo 4; s. 1516 - 1534
Hlavní autoři:	Mansouri, Akbar, Alem-Tabriz, Akbar
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Philadelphia Taylor & Francis 16.02.2024 Taylor & Francis Ltd
Témata:	Algorithms attitude determination and control system Control systems Exact solutions Heuristic methods Linear programming Mathematical analysis Mathematical models Mixed integer Nonlinear programming Optimization Optimization exact method Redundancy redundancy allocation problem Redundant components reliability engineering satellite Satellite attitude control Satellite tracking
ISSN:	0361-0926, 1532-415X
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Abstract	The redundancy allocation problem is to find an optimal allocation of redundant components by considering the set of resources and cost constraints. In this research, the satellite attitude determination and control system is studied and its components is introduced, then the reliability of this system is modeled and optimized based on a mathematical approach based on the redundancy allocation. The model studied in this paper is about the structure of a series-parallel system that is in the exact mode of a satellite attitude determination and control system. In this paper, a new approach for modeling and optimization is presented. The mathematical model presented in this paper is into the class of mixed integer non-linear programming (MINLP). Solving these problems is very important for various researchers due to the high mathematical complexity. In this research, a heuristic method is used to the problem exact solution, the results of which have been reported.
AbstractList	The redundancy allocation problem is to find an optimal allocation of redundant components by considering the set of resources and cost constraints. In this research, the satellite attitude determination and control system is studied and its components is introduced, then the reliability of this system is modeled and optimized based on a mathematical approach based on the redundancy allocation. The model studied in this paper is about the structure of a series-parallel system that is in the exact mode of a satellite attitude determination and control system. In this paper, a new approach for modeling and optimization is presented. The mathematical model presented in this paper is into the class of mixed integer non-linear programming (MINLP). Solving these problems is very important for various researchers due to the high mathematical complexity. In this research, a heuristic method is used to the problem exact solution, the results of which have been reported.
Author	Alem-Tabriz, Akbar Mansouri, Akbar
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SubjectTerms	Algorithms attitude determination and control system Control systems Exact solutions Heuristic methods Linear programming Mathematical analysis Mathematical models Mixed integer Nonlinear programming Optimization Optimization exact method Redundancy redundancy allocation problem Redundant components reliability engineering satellite Satellite attitude control Satellite tracking
Title	Redundancy allocation optimizing in the satellite attitude determination and control system based on the exact solution algorithm
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