摘要: Thirty two channels of flight data were recorded to validate a mathematical model of an R.A.N. Sea King Mk. 50 helicopter. Described is the calibration procedure used for each channel. (Author)
| 作者 | Hourigan, D. T. | ||
|---|---|---|---|
| 原报告号 | ADA096587 | 总页数 | 44 |
| 报告类别/文献类型 | AD / NTIS科技报告 | ||
| 关键词 | Flight Helicopters Mathematical models Validation Data acquisition Aerodynamic characteristics Calibration Pitch(Motion) Roll Yaw Sideslip Airspeed Static pressure Altitude Acceleration Radio altimeters Recording systems Data transmission systems | ||
