Integrated Energy And Power Management: Validation Testing For Aerospace Vehicles

Abstract

The structured technical and organizational approach to integrated dynamic energy and power management research is outlined from an integrated vehicle and dynamic subsystem/component perspective. This approach combines physics-based and statistical modeling and component and system validation testing on baseline airframe(s) in a flight simulated environment. It is concluded that experimental data of individual system component tests are not alone sufficient. Laboratory tests on an integrated airframe with interacting subsystems are needed to properly define requirements for effective validation testing needed to support robust model-based engineering and life-cycle growth management. The objective is to develop and demonstrate a robust validation testing approach that transcends beyond the component-only focus to one that addresses the vehicle in its entirety and throughout the vehicle life-cycle.

Publication Date

1-1-2016

Publication Title

AIAA Modeling and Simulation Technologies Conference

Document Type

Article; Proceedings Paper

Personal Identifier

scopus

Socpus ID

84957991285 (Scopus)

Source API URL

https://api.elsevier.com/content/abstract/scopus_id/84957991285

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