• 主题
高级搜索  >
历史搜索 清空历史
首页> 美国政府科技报告 >Modeling Interactions Between Flexible Flapping Wing Spars, Mechanisms, and Drive Motors
【24h】

Modeling Interactions Between Flexible Flapping Wing Spars, Mechanisms, and Drive Motors

机译：模拟柔性扑翼翼梁，机构和驱动马达之间的相互作用

获取原文
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

A system of dynamical equations is presented that allow micro air vehicle (MAV) or- nithopter designers to match drive motors to loads produced by exible apping wing spars. The model can be used to examine the coupled system-level behavior of brushed DC motors, gear trains, and any number of linkages and exible wing spars. A Lagrangian approach is used to derive the governing di erential equations of motion for a class of or- nithopter drive systems. Methods used to determine parametric constants contributing to generalized force components, which cannot be derived from first principles, are described. An example is presented where simulation results are compared to experimental measure- ments. The results show that the di erential equations correctly predict major trends in observed motor speed and wing spar structural deformation over the course of each wingbeat. The results show that when pairing ight-weight motors and wings, signi cant variations in drive motor speed occur throughout each wingbeat. It is shown that cou- pling between motor speed, wing loads, and structural exibility cause the aerodynamic forces encountered by the wing spars to depart from those predicted by rigid-spar and constant-velocity-motor-based kinematic simulations.

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

  • 客服微信

  • 服务号