| 摘要 |
A method of high fidelity modeling an electrical power system of an aircraft, includes among other things, identifying electrical (110), mechanical (112), thermal (114), and EMI characteristics (116) of the electrical power system; applying at least one circuit-based solver (120) 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 (122,132,134,136,138) to model the remaining electrical, mechanical, thermal, and EMI characteristics. |
