| タイトル | STABCAR: A program for finding characteristic root systems having transcendental stability matrices |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840019393 |
| 著者（英） | Adams, W. M., Jr.; Peele, E. L.; Newsom, J. R.; Tiffany, S. H. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1984-06-01 |
| 言語 | eng |
| 内容記述 | STABCAR can be used to determine the characteristic roots of flexible, actively controlled aircraft, including the effects of unsteady aerodynamics. A modal formulation and a transfer-matrix representation of the control system are employed. Operable in either a batch or an interactive mode, STABCAR can provide graphical or tabular output of the variation of the roots with velocity, density, altitude, dynamic pressure or feedback gains. Herein the mathematical model, program structure, input requirements, output capabilities, and a series of sample cases are detailed. STABCAR was written for use on CDC CYBER 175 equipment; modification would be required for operation on other machines. |
| NASA分類 | COMPUTER PROGRAMMING AND SOFTWARE |
| レポートNO | 84N27461
NASA-TP-2165
NAS 1.60:2165
L-14861 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/159181 |
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