| タイトル | Controls for agility research in the NASA High-Alpha Technology Program |
| 著者（英） | Bundick, W. T.; Pahle, Joseph W.; Foster, John V. |
| 著者所属（英） | NASA Langley Research Center; NASA Dryden Flight Research Center |
| 発行日 | 1991-09-01 |
| 言語 | eng |
| 内容記述 | The research process being used to develop control law design methodologies and guidelines in the NASA High-Alpha Technology Program are discussed. This step-by-step process consists of four basic elements: (1) control law architecture definition and linear synthesis, (2) nonlinear batch simulation, (3) piloted simulation evaluation, and (4) flight test validation. This paper discusses the research tools being used in this effort and provides a status report on design methodologies and guidelines being developed for each of these elements. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | 92A39984
SAE PAPER 912148 |
| 権利 | Copyright |
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