Actions for Integrated Application of Active Controls (IAAC) technology to an advanced subsonic transport project : Test act system description

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Integrated Application of Active Controls (IAAC) technology to an advanced subsonic transport project : Test act system description

Published
Dec 1, 1983.
Physical Description
1 electronic document
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The engineering and fabrication of the test ACT system, produced in the third program element of the IAAC Project is documented. The system incorporates pitch-augmented stability and wing-load alleviation, plus full authority fly-by-wire control of the elevators. The pitch-augmented stability is designed to have reliability sufficient to allow flight with neutral or negative inherent longitudinal stability.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19860004807.
Accession ID: 86N14277.
NAS 1.26:172221.
NASA-CR-172221.
D6-51825.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15703601