| タイトル | Simulation evaluation of two VTOL control/display systems in IMC approach and shipboard landing |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850006532 |
| 著者（英） | Merrick, V. K. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1984-12-01 |
| 言語 | eng |
| 内容記述 | Two control/display systems, which differed in overall complexity but were both designed for VTOL flight operations to and from small ships in instrument meteorological conditions (IMC), were tested using the Ames Flight Simulator for Advanced Aircraft (FSAA). Both systems have attitude command in transition and horizontal-velocity command in hover; the more complex system also has longitudinal-acceleration and flightpath-angle command in transition, and vertical-velocity command in hover. The most important overall distinction between the two systems for the viewpoint of implementation is that in one - the more complex - engine power and nozzle position are operated indirectly through flight controllers, whereas in the other they are operated directly by the pilot. Simulated landings were made on a moving model of a DD 963 Spruance-class destroyer. Acceptable transitions can be performed in turbulence of 3 m/sec rms using either system. Acceptable landings up to sea state 6 can be performed using the more complex system, and up to sea state 5 using the other system. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 85N14841
NAS 1.15:85996
A-9838
NASA-TM-85996 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/157629 |
