An MBSE Framework to Identify Regulatory Gaps for Electrified Transport Aircraft

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

A typical aircraft certification process consists of obtaining a type, production, airworthiness, and continued airworthiness certificates. During this process, a type certification plan is created that includes the intended regulatory operating environment, the proposed certification basis, means of compliance, and a list of documentation to show compliance. Earlier work by the authors demonstrated a model-based framework for the management of these certification artifacts for normal category airplanes. Presently, it is expanded and adapted to consider certification for transport category airplanes regulated under 14 CFR Part 25, providing clear transparency and traceability between the text of the regulations and imposed requirements, contextual information, and specified test activities. In particular, a capability to identify potential gaps in the applicability of regulations for novel architectures such as electrified aircraft is proposed. This capability, based on mismatches between the functional intent and the corresponding prescribed physical implementation, is developed. A sample implementation of the proposed capability is presented for a notional electrified powertrain aircraft architecture.

Authors

• Stephen Glinski Georgia Institute of Technology
• Bijan Fazal Georgia Institute of Technology
• Evan D. Harrison Georgia Institute of Technology
• Mayank V. Bendarkar Georgia Institute of Technology
• Taylor Fields Georgia Institute of Technology
• Elena Garcia Georgia Institute of Technology
• Dimitri N. Mavris Georgia Institute of Technology

Keywords

• electrified transport aircraft
• aircraft certification
• airworthiness
• type certification
• electrified propulsion
• Model-based Systems Engineering (MBSE)
• Regulatory Gap Analysis