The invention discloses a
civil aviation element
configuration optimization method based on mixed integer
dynamic programming. The method comprises the following steps: S1, constructing a Chinese
civil aviation core element and carbon emission spatial-temporal characteristic
database; s2, establishing a mixed integer
dynamic programming model with the purpose of minimizing the total cost of the
system in the
programming period; and S3, establishing decision variables, constraint conditions and a fusion solution
algorithm framework required by the mixed integer
dynamic programming model. And S4, based on the fusion solution
algorithm framework, solving the mixed integer dynamic
programming model by using a mathematical
programming solver integrated with a
robust optimization module so as to obtain a
civil aviation core element dynamic configuration scheme which is optimal in total
system cost in multiple periods in the future and meets the uncertainty scene. According to the method provided by the invention, a multi-
source data fusion
algorithm is optimized, a carbon emission measuring and calculating method is deepened, and
solver parameters are adjusted, so that the collaborative requirements of improving the operation efficiency and reducing the carbon emission from the perspective of carbon cost are met.