Reliability Approach to Optimal Thruster Configuration Design for Spacecraft Attitude Control Subsystem
An optimal thruster configuration for attitude control subsystem of a spacecraft is presented in this paper. The optimal configuration is designed according to minimum number of required thrusters for satisfying desired reliability with specific redundancy level. The genetic algorithm is employed fo...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Departamento de Ciência e Tecnologia Aeroespacial
2020-05-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | https://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e2320.pdf |