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   悬停控制器 的翻译结果: 查询用时:0.191秒
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悬停控制器
相关语句
  hover controller
     Hover Controller Design for a Certain Helicopter
     某型直升机悬停控制器设计研究
  “悬停控制器”译为未确定词的双语例句
     The design method of the robust controller combined with the controller of the helicopter hover is given in detail, and the computer simulation results well explain the function of the robust controller in the example.
     详细叙述了鲁棒控制器结合悬停控制器的设计方法,并用仿真结果说明了鲁棒控制器在本算例中所起的作用
短句来源
     Considering the nonlinearity of FMAV, it is also considerate to analyze the feasibility of applying modern control theory to the control system of FMAV. This is done by designing the locus tracking system and optimal control system oflongitudinal locomotion. Moreover, a hovering controller is also designed, validating the maneuverability of FMAV. Finally, an adaptive critical control system based on neural network is developed, validating the feasibility of applying neural network to solve the nonlinear problems of vehicles.
     针对微型扑翼飞行器的非线性特点,本文还分析了将一些现代的控制理论应用到飞行器控制上的可行性,设计了纵向运动的轨迹跟踪系统和最优控制系统,还设计了微型扑翼飞行器的悬停控制器,验证了飞行器的机动性,最后利用神经网络技术设计了自适应校正控制系统,验证了用神经网络解决飞行器非线性问题的可行性和优越性。
短句来源
     The scheme does not change the original structures of the velocity loop, adding only a robust controller as an outer loop for the original velocity loop. For this reason, the new scheme improves the robust properties of the variation of the parameters in the helicopter hover.
     在直升机悬停控制器原速度回路的基础上增加鲁棒控制器,可提高直升机悬停参数变化的鲁棒性能。
短句来源
  相似匹配句对
     Hover Controller Design for a Certain Helicopter
     某型直升机悬停控制器设计研究
     Type U Crate Controller
     U型机箱控制器
短句来源
     A Study of the Controller of Stepping Motors
     步进电机控制器的研究
短句来源
     Recognition of a Hovering Helicopter
     悬停直升机的识别
短句来源
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A new control scheme for helicopter hover is developed. The scheme does not change the original structures of the velocity loop, adding only a robust controller as an outer loop for the original velocity loop. For this reason, the new scheme improves the robust properties of the variation of the parameters in the helicopter hover. The design method of the robust controller combined with the controller of the helicopter hover is given in detail, and the computer simulation results well explain the function of...

A new control scheme for helicopter hover is developed. The scheme does not change the original structures of the velocity loop, adding only a robust controller as an outer loop for the original velocity loop. For this reason, the new scheme improves the robust properties of the variation of the parameters in the helicopter hover. The design method of the robust controller combined with the controller of the helicopter hover is given in detail, and the computer simulation results well explain the function of the robust controller in the example.

提出一种改进直升机悬停性能的控制方案。在直升机悬停控制器原速度回路的基础上增加鲁棒控制器,可提高直升机悬停参数变化的鲁棒性能。详细叙述了鲁棒控制器结合悬停控制器的设计方法,并用仿真结果说明了鲁棒控制器在本算例中所起的作用

>=This paper studies the hovering controller for a helicopter. The linear helicopter equation of motion is introduced. The digital simulation models are established as well. The parameters mapping method is developed to search the best available hover controller parameters in all kinds of the flight states. Simulation results are given to demonstrate the effectiveness of the designed controllers. The hover maneuver is passed the test flight using the proposed control law.

本文对某型直升机悬停控制器进行设计研究,根据建立的直升机六自由度线性化动力学方程和直升机全数字仿真模型,提出了参数映射法选择所设计控制器的控制参数。悬停控制律经过全数字仿真验证后,编写了控制律软件并装入飞行控制计算机上机试飞,试飞结果证明作者设计的控制器安全有效。

 
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