METHOD FOR HIGH FIDELITY MODELING OF AN AIRCRAFT ELECTRICAL POWER SYSTEM

摘要

A method of high fidelity modeling an electrical power system of an aircraft, includes among other things, identifying electrical, mechanical, thermal, and EMI characteristics of the electrical power system; applying at least one circuit- based solver to model to at least one of the electrical characteristics; and applying, simultaneously with the circuit-based solver and in real-time, a field-based solver to model the remaining electrical, mechanical, thermal, and EMI characteristics.