Microcomputer based solid state crash data recorder for military aircraft

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Authors
Albertolli, William Ramon
Subjects
Flight data recording
Nonvolatile solid state memory
Microcomputers
Aircraft accident investigation
Advisors
Kodres, U.R.
Date of Issue
1976-12
Date
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
The design, breadboard implementation, and functional testing of a Crash Data Recorder for military aircraft is reported. A microcomputer is used to analyze the flight parameters, reduce redundant data, and record only significant information to be used in post-crash analysis. Nonvolatile solid state memory is used as the recording medium. Functional tests indicate that the solid state recorder's reliability is higher than that of mechanical magnetic tape recorders while cost, weight, size, and required maintenance are greatly reduced. The microcomputer provides an expansion capability for future applications of the flight recorder. Research and development, structural history, maintenance analysis, and training are areas where the Crash Data Recorder can also serve as an analytical tool. Continued research in this subject is highly recommended.
Type
Thesis
Description
Series/Report No
Department
Aeronautical Engineering
Organization
Naval Postgraduate School
Identifiers
NPS Report Number
Sponsors
Funding
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
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