Abstract
The article considers an optimization of a spacecraft component. The choice of length of the power supply was carried out using a genetic algorithm. The main purpose was decreasing the maximum voltage amplitude in the power supply bus. As an excitation we used a differential excitation of a trapezoidal pulse. Comparison of the results of signal simulation after optimization for two approaches is presented, that differed by various numbers of chromosomes and populations. It was found that the two approaches are not differ significantly in the simulation results. We decreased the maximum voltage amplitude by 270 times with using the genetic algorithm.
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