1. A method for generating a solution for sequencing the specifications of an aircraft computer, wherein the method comprises: an automatic analysis of the specifications constituted by nodes with a simplification and distribution of these nodes into at least two types of nodes, this distribution by type of node being a function of criteria and/or constraints of each node, an automatic assigning of these nodes in repetitive sub-cycles of processing tasks in order to obtain a substantially uniform distribution of the tasks, and an automatic obtaining of a sequencing solution.