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超空泡航行体的变结构控制器设计
  • 期刊名称:兵工学报. 2009, 30(8): 1147-1152
  • 时间:0
  • 分类:TP29[自动化与计算机技术—控制科学与工程;自动化与计算机技术—检测技术与自动化装置]
  • 作者机构:[1]哈尔滨工业大学航天学院,黑龙江哈尔滨150001
  • 相关基金:国家自然科学基金资助项目(10802026);高等学校博士点基金资助项目(20080213003)
  • 相关项目:超空泡航行体动力学建模与控制研究
中文摘要:

超空泡航行体由于浮力缺失以及尾部滑行力的出现,使航行体具有了尾拍、结构振动和非线性等复杂的运动特征,给超空泡航行体的运动稳定控制设计造成了极大的困难。通过分析作用在超空泡航行体上的流体动力,推导出了超空泡下潜一俯仰面运动数学模型。依据对该模型开环时的系统特性分析,针对开环系统的不稳定性,设计了基于改进型指数趋近率的变结构控制器,并进行了数学仿真。仿真结果表明,该闭环系统响应快速,具有良好的稳定性能。

英文摘要:

With the loss of the buoyancy and the occurrence of the planing force being brought by supercavitation, the supercavitating vehicles confront complicate motion characters, such as tail-slap, structural vibrations and nonlinearity. These problems bring great difficulties for stability control design, Through analyzing the hydrodynamic forces acting on supercavitating vehicles, a dive-pitch-plane dynamics model for supercavitating vehicle was presented. According to open-loop system response, and due to the instability of the system, a variable-structure controller based on improved exponent approaching law was designed, and mathematical simulation was performed for supercavitating vehicles with the controller. The simulation result demonstrates that the closed-loop system responds rapidly and has good performance.

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