| タイトル | Simulation of Dynamics of a Flexible Miniature Airplane |
| 本文（外部サイト） | http://hdl.handle.net/2060/20110015081 |
| 著者（英） | Waszak, Martin R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2005-08-01 |
| 言語 | eng |
| 内容記述 | A short report discusses selected aspects of the development of the University of Florida micro-aerial vehicle (UFMAV) basically, a miniature airplane that has a flexible wing and is representative of a new class of airplanes that would operate autonomously or under remote control and be used for surveillance and/or scientific observation. The flexibility of the wing is to be optimized such that passive deformation of the wing in the presence of aerodynamic disturbances would reduce the overall response of the airplane to disturbances, thereby rendering the airplane more stable as an observation platform. The aspect of the development emphasized in the report is that of computational simulation of dynamics of the UFMAV in flight, for the purpose of generating mathematical models for use in designing control systems for the airplane. The simulations are performed by use of data from a wind-tunnel test of the airplane in combination with commercial software, in which are codified a standard set of equations of motion of an airplane, and a set of mathematical routines to compute trim conditions and extract linear state space models. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | LAR-16414-1 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/270395 |
