摘要
Unmanned aerial vehicles (UAV) are playing important roles in many fields. The configuration and control of an unmanned tandem helicopter using models for the rotor and the helicopter were analyzed. The model was used to relate the control parameters to the helicopter flight characteristics and to simulate real-time flight for display on a PC. The simulated control results approximated real helicopter flight for small disturbances.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 83-85+93 |
| 期刊 | Qinghua Daxue Xuebao/Journal of Tsinghua University |
| 卷 | 43 |
| 期 | 1 |
| 出版状态 | 已出版 - 1月 2003 |
| 已对外发布 | 是 |
学术指纹
探究 'Unmanned tandem helicopter simulation' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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