| タイトル | A mathematical force and moment model of a UH-1H helicopter for flight dynamics simulations |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770024231 |
| 著者（英） | Corliss, L. D.; Talbot, P. D. |
| 著者所属（英） | NASA Ames Research Center|Army Air Mobility Research and Development Lab. |
| 発行日 | 1977-06-01 |
| 言語 | eng |
| 内容記述 | A model of a UH-1H helicopter was developed to support flight simulations and for developmental work on an avionics system known as V/STOLAND system. Equations and numerical values of constants used to represent the helicopter are presented. Responses to stop inputs of the cyclic and collective controls are shown and compared with flight test data for a UH-1H. The model coefficients were adjusted in an attempt to get a consistant match with the flight time histories at hover and 60 knots. Response matching was obtained at 60 knots, but the matching at hover was not as successful. Pilot evaluations of the model, both fixed and moving base, were made. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 77N31175
A-7080
NASA-TM-73254 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/181325 |
