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Integrated application of active controls (iaac) technology to an advanced subsonic transport project: test act system description
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1983 |
| Description | 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. |
| File Size | 16724958 |
| Page Count | 326 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860004807 |
| Archival Resource Key | ark:/13960/t7xm34z4k |
| Language | English |
| Publisher Date | 1983-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Subsonic Speed Fly By Wire Control Redundancy Automatic Flight Control Automatic Control Stability Augmentation Aircraft Engines Acee Program Active Control Wing Loading Aerodynamic Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
