摘要: System-identification methods compose a mathematical model, or series of models,from measurements of inputs and outputs of dynamic systems. The extracted models allow the characterization of the response of the overall aircraft or... 展开
作者 | Tischler, M. B. | ||
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原报告号 | N9613229 | 总页数 | 22 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft design Computerized simulation Control systems design Dynamicresponse Fixed wings Flight control Flight tests Mathematical models Performance tests Rotary wing aircraft System identification Vertical landing Vertical takeoff Actuator |