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F-14 modeling study
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Levison, W. H. Baron, S. |
| Copyright Year | 1984 |
| Description | Preliminary results in the application of a closed loop pilot/simulator model to the analysis of some simulator fidelity issues are discussed in the context of an air to air target tracking task. The closed loop model is described briefly. Then, problem simplifications that are employed to reduce computational costs are discussed. Finally, model results showing sensitivity of performance to various assumptions concerning the simulator and/or the pilot are presented. |
| File Size | 1977015 |
| Page Count | 100 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840017633 |
| Archival Resource Key | ark:/13960/t9q28rh7q |
| Language | English |
| Publisher Date | 1984-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance F-14 Aircraft Pilot Performance Feedback Optimal Control Aircraft Pilots Models Man Machine Systems Tracking Position Flight Simulation 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 |
