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A flight-test evaluation of a go-around control system for a twin engine powered-lift stol airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hardy, G. H. Watson, D. M. |
| Copyright Year | 1983 |
| Description | An automatic go-around control system was evaluated on the Augmentor Wing Jet Short Takeoff and Landing (STOL) Research Airplane (AWJSRA) as part of a study of an automatic landing system for a powered-lift STOL airplane. The results of the evaluation indicate that the go-around control system can successfully transition the airplane to a climb configuration from any initiation point during the glide-slope track or the flare maneuver prior to touchdown. |
| File Size | 967775 |
| Page Count | 21 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840003110 |
| Archival Resource Key | ark:/13960/t9n34pk0m |
| Language | English |
| Publisher Date | 1983-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Flight Tests Aircraft Instruments Landing Aids Short Takeoff Aircraft Glide Paths Flight Control Powered Lift Aircraft Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |