DocumentCode
1486339
Title
Man-machine interaction in aerospace control systems
Author
Towill, D.R.
Volume
50
Issue
9
fYear
1980
fDate
9/1/1980 12:00:00 AM
Firstpage
447
Lastpage
458
Abstract
The Multi-Role Combat Aircraft Tornado is probably the most spectacular example to date of a complex man-machine system in which design and manufacture are widely dispersed. Even sub-assemblies of this system are extremely complex relative to the technology of just a few years ago. This makes life extremely difficult for an engineer involved in the procurement of the sub-assembly, especially as the overall objective can soon be submerged in a mass of detail. Starting with a review of desirable dynamic properties of the machine, as seen by the man, typical human operator transfer functions which have found use in closed-loop control system design are presented. Some ways in which microelectronics can reduce pilot work load are then discussed with the object of conveying to the design engineer some of the reasoning behind the performance specification he is trying to meet. Examples include helicopter stability augmentation systems and spacecraft terminal phase control.
Keywords
aerospace control; aircraft instrumentation; Tornado aircraft; aerospace control system; closed loop control system; helicopter stability augmentation systems; human operator transfer functions; man machine interaction; spacecraft terminal phase control;
fLanguage
English
Journal_Title
Radio and Electronic Engineer
Publisher
iet
ISSN
0033-7722
Type
jour
DOI
10.1049/ree.1980.0069
Filename
5269754
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