Integrated Flight Test Data System With Real-Time Graphic Display

690678

10/06/1969

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
Future flight test programs of sophisticated commercial and military aircraft, requiring a multitude of parameter measurements and fast data turn-around-time, dictate the need for a new approach to data acquisition and processing. This paper shows how these goals will be met using a total systems approach to automate the process while keeping the “man in the loop”.
The airborne system includes universal signal conditioning, digitizing, high packing density serial tape recording, and simultaneous telemetry transmission for up to 400 data channels. The ground station permits real-time and nonreal-time processing of multiple data streams without the need for editing or preprocessing procedures. The principal features of the ground station include advanced data acquisition front ends, a third generation computer, and cathode ray tube graphic displays of data in engineering units which permit on-line interactive data processing by the flight test engineer.
Meta TagsDetails
DOI
https://doi.org/10.4271/690678
Pages
10
Citation
Strom, J., and Crowley, L., "Integrated Flight Test Data System With Real-Time Graphic Display," SAE Technical Paper 690678, 1969, https://doi.org/10.4271/690678.
Additional Details
Publisher
Published
Oct 6, 1969
Product Code
690678
Content Type
Technical Paper
Language
English