Effects of gyroscopic coupling and countertorque in a fixed-wing nano air vehicle
For the nonlinear equations of motion of the nano air vehicle, including the gyroscopic coupling and countertorque generated by the propulsion system, a linear state-space model is developed for analyzing the effects of gyroscopic coupling and countertorque on the dynamic behavior of the nano air ve...
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| Main Authors: | , , |
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| 格式: | Article |
| 語言: | English |
| 出版: |
2019
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| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/106668 http://hdl.handle.net/10220/50044 http://dx.doi.org/10.2514/1.C034280 |
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