Abstract
Aiming at the disadvantages of traditional process of achieving the RMS requirements, which the less of monitoring points, hardly controlling this process and easily leading to the iterative design, etc. are included. A methodology, Process of Requirement Integrated & Dynamic Espial (PRIDE), for the achievement of equipment RMS requirements was proposed at first, and its framework was given subsequently. Then a set of elements structure of PRIDE, based on the monitoring space model of the overall system, overall process and overall properties (three-A), was built, which lay the foundation for the realization of the PRIDE in achieving equipment RMS requirements. Finally, a certain type of aircraft was taken as the case to verify the feasibility of the monitoring elements structure.
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