| Citation: | HUO Lin, FEI Simiao. Flight management system redundancy optimization method based on genetic algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(7): 1306-1312. doi: 10.13700/j.bh.1001-5965.2016.0512(in Chinese)
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Aircraft management system is an important part to guarantee flight safety, and redundancy design is the main method to improve the safety of the system. The redundancy design, however, is constrained by the budget (economy) in the design and manufacture and the consumption of the maintenance support resources (reliability). According to the safety, basic reliability and economy models of aircraft management system, a redundancy configuration optimization method was proposed by using the improved integer optimal genetic algorithm, with safety as the objective, and basic reliability and economy as the constraint. Then an example was taken to show its effectiveness to the complex system redundancy optimization. The sensitivity analysis shows that the safety optimal value declines with the increase of the basic reliability lower bound, and rises with the increase of the economy upper bound. For two constraints on the optimization of the objective competitive constraints, at the same time only one constraint condition plays a major constraint role. These two constraint conditions play a role in the competition, and at the same time there is only one main constraint.
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