变后掠翼
- Variable sweep wing;【航空】variable swept back wing
变后掠翼-
一种无人机变后掠翼机构的设计与仿真研究
Study of a Variable Wing Sweep Mechanism Design for Unmanned Air Vehicle
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本文结合国家自然科学基金项目（61273090），对可不对称变后掠翼飞行器的多刚体建模和飞行控制进行了深入的研究，并介绍了相关硬件实验平台的工作进展。
Our research is supported by the National Natural Science Foundation of China ( Grant No61273090 ) . In this paper , we propose an intensive study on multi-body dynamic modelling and flight control of asymmetric variable sweep aircrafts , and report the progress of our UAV hardware experiment platform .