摘要
A new method was presented for the dynamic modeling and control system designing of a morphing micro aircraft with variable sweep. Through operating point selecting, aerodynamic calculation and data fitting, dynamic model of the morphing aircraft was established. According to the characteristics of dynamic model, a flight control system design method was put forward based on parameter space approach for morphing aircraft. With computer aided design method, a longitudinal control system was designed. The simulation results show that the designed public fixed-gain controller can make the morphing aircraft have required dynamic characteristics in different flight stages, and show its feasibility and practicability.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 796-800 and 830 |
| 期刊 | Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology |
| 卷 | 34 |
| 期 | 8 |
| 出版状态 | 已出版 - 1 8月 2014 |