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   超小型旋翼机 的翻译结果: 查询用时:0.205秒
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超小型旋翼机
相关语句
  subminiature rotorcraft
     Output Tracking Control Design of Subminiature Rotorcraft
     超小型旋翼机系统的输出跟踪控制器设计
短句来源
     A model for the nonlinear dynamics of a subminiature rotorcraft is established.
     建立了超小型旋翼机系统的非线性参数化模型.
短句来源
     Then according to horizontal turning,a diagonal re-cursive neural network was used to compensate the model error between the mechanism model and the real nonlinear model, thus the hybrid model of a subminiature rotorcraft in horizontal turning was achieved.
     然后针对转弯运动,采用对角回归网络来补偿机理模型与非线性模型之间的误差,从而获得超小型旋翼机系统的平面转弯运动的混合模型。
短句来源
     Modeling of a Subminiature Rotorcraft in Horizontal Turning by Using NN-Compensation
     超小型旋翼机平面转弯运动的神经网络补偿建模
短句来源
     Identification and Simulation of a Subminiature Rotorcraft in Hover
     超小型旋翼机系统悬停状态的辨识仿真研究
短句来源
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  “超小型旋翼机”译为未确定词的双语例句
     Simulation results show that the subspace method can identify the physical parametric attitude dynamics of miniature rotorcraft in hover accurately,and thus some physical parameters which cannot be calculated or measured precisely,can be deduced.
     仿真结果表明:子空间方法可以较准确地辨识所推导的超小型旋翼机系统悬停状态的线性物理参数模型,从而能获得系统的一些难以准确计算或测量的主要物理参数.
短句来源
  相似匹配句对
     Output Tracking Control Design of Subminiature Rotorcraft
     超小型旋翼机系统的输出跟踪控制器设计
短句来源
     A model for the nonlinear dynamics of a subminiature rotorcraft is established.
     建立了超小型旋翼机系统的非线性参数化模型.
短句来源
     A Multi-functional Gyroplane
     新型多功能旋翼机
短句来源
     Superminiature Machining Unit
     超小型加工装置
短句来源
     Nissan's Hypermini Electric Vehicles
     日产超小型电动汽车Hypermini
短句来源
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A model for the nonlinear dynamics of a subminiature rotorcraft is established.Through the linearization of the nonlinear dynamics,the linear time-invariant attitude dynamics with physical parameter of the subminiature rotorcraft in hover is obtained.A subspace-based state space system identification method is applied to identify the model of rotorcraft in hover.Simulation results show that the subspace method can identify the physical parametric attitude dynamics of miniature rotorcraft in hover accurately,and...

A model for the nonlinear dynamics of a subminiature rotorcraft is established.Through the linearization of the nonlinear dynamics,the linear time-invariant attitude dynamics with physical parameter of the subminiature rotorcraft in hover is obtained.A subspace-based state space system identification method is applied to identify the model of rotorcraft in hover.Simulation results show that the subspace method can identify the physical parametric attitude dynamics of miniature rotorcraft in hover accurately,and thus some physical parameters which cannot be calculated or measured precisely,can be deduced.

建立了超小型旋翼机系统的非线性参数化模型.通过把非线性模型在悬停点线性化,得到用物理参数描述的系统姿态运动的线性模型;基于其离散状态空间模型,采用子空间方法进行线性系统识别.仿真结果表明:子空间方法可以较准确地辨识所推导的超小型旋翼机系统悬停状态的线性物理参数模型,从而能获得系统的一些难以准确计算或测量的主要物理参数.

The dynamics of a subminiature rotorcraft was given including flybar’s flapping.Further simplification of the control design process could be realized by dividing the rotorcraft dynamics into translational dynamics and attitude dynamics by using singular perturbation theory.The output tracking control design of the rotorcraft based on nonlinear inverse dynamics was described.The simulation results show that a desired trajectory can be tracked and the proposed control scheme is proved to result in global exponential...

The dynamics of a subminiature rotorcraft was given including flybar’s flapping.Further simplification of the control design process could be realized by dividing the rotorcraft dynamics into translational dynamics and attitude dynamics by using singular perturbation theory.The output tracking control design of the rotorcraft based on nonlinear inverse dynamics was described.The simulation results show that a desired trajectory can be tracked and the proposed control scheme is proved to result in global exponential stability and convergence in the trajectory error.

针对复杂的超小型旋翼机系统,利用牛顿-欧拉方法建立了其系统动力学模型,包括了希勒翼的动力学;为了简化控制器设计,利用奇异扰动理论,把复杂的动力学模型降阶为两个子系统,即平移动力学和姿态动力学;采用非线性逆动力学设计了输出跟踪控制器。仿真结果表明该控制器能够跟踪理想的运动轨迹,并能达到稳定的内部姿态和有界的控制输入。

A hybrid modeling method of a subminiature rotorcraft in horizontal turning had been proposed by using mechanism model and NN-compensation.First,the nonlinear dynamics of a subminiature rotorcraft was established.Through linearization of the nonlinear dynamics on the trim point,the linear time-invariant mechanism model in horizontal turning had been obtained.Then according to horizontal turning,a diagonal re-cursive neural network was used to compensate the model error between the mechanism model and the real...

A hybrid modeling method of a subminiature rotorcraft in horizontal turning had been proposed by using mechanism model and NN-compensation.First,the nonlinear dynamics of a subminiature rotorcraft was established.Through linearization of the nonlinear dynamics on the trim point,the linear time-invariant mechanism model in horizontal turning had been obtained.Then according to horizontal turning,a diagonal re-cursive neural network was used to compensate the model error between the mechanism model and the real nonlinear model, thus the hybrid model of a subminiature rotorcraft in horizontal turning was achieved.Simulation results show that the hybrid model has higher accuracy than that of mechanism model and the obtained compensated-NN has high ability of generalization.

采用神经网络补偿机理模型法进行超小型旋翼机系统的平面转弯运动建模。首先建立系统的非线性参数化模型,通过把非线性模型在平衡点线性化,得到描述系统平面转弯运动的线性机理模型;然后针对转弯运动,采用对角回归网络来补偿机理模型与非线性模型之间的误差,从而获得超小型旋翼机系统的平面转弯运动的混合模型。仿真结果表明,该混合模型比单纯机理模型有更高的精度,且所获得的补偿神经网络具有很强的泛化能力。

 
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