首页> 外文会议>2010 International Conference on Computer Application and System Modeling >Dynamics analysis and simulation of 9 DOF unmanned powered parachute based on Kane method
【24h】

Dynamics analysis and simulation of 9 DOF unmanned powered parachute based on Kane method

机译:基于凯恩法的9自由度无人动力降落伞动力学分析与仿真

获取原文

摘要

A formulation based on Kane Equation and kinematics of unmanned powered parachute was educed, which includes free and constraintmode. The velocities of unmanned powered parachute's parafoil and vehicalvehicle which linked to base joint were chosen as generalized velocities. The partial velociy and the partial angular velocity of parafoil and vehical were educed. Develop a 9DOF dynamics model of a unmanned powered parachute. The numerical simulation of the dynamics was carried out by using MATLAB software.The simulation results show that the unmanned powered parachute has passive and constraint characteristics.The dynamics can provide theoretical bases for analysis and simulation of the umanned powered prachute control and so forth.
机译:提出了一种基于凯恩方程和无人动力降落伞运动学的公式,包括自由和约束模式。选择无人动力降落伞的副翼和与基础接头连接的车辆的速度作为广义速度。得出了翼型和车辆的局部速度和局部角速度。开发无人动力降落伞的9DOF动力学模型。利用MATLAB软件对动力学进行了数值模拟,仿真结果表明,该无人机具有被动和约束特性。该动力学特性可以为分析,仿真无人机动力控制等提供理论依据。

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