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Bandwidth and simduce as simulator fidelity criteria
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Key, David |
| Copyright Year | 1992 |
| Description | The potential application of two concepts from the new Handling Qualities Specification for Military Rotorcraft was discussed. The first concept is bandwidth, a measure of the dynamic response to control. The second is a qualitative technique developed for assessing the visual cue environment the pilot has in bad weather and at night. Simulated Day Usable Cue Environment (SIMDUCE) applies this concept to assessing the day cuing fidelity in the simulator. |
| File Size | 666955 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930021501 |
| Archival Resource Key | ark:/13960/t6j14zn9q |
| Language | English |
| Publisher Date | 1992-04-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Dynamic Response Cues Flight Conditions Night Daytime Helicopters Flight Simulators Bandwidth Visual Stimuli Rotary Wing Aircraft Flight Simulation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |