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三环驱动轴对称推力矢量喷管逆运动学分析

赵志刚 李建鹏 刘洋 李维维

赵志刚, 李建鹏, 刘洋, 李维维. 三环驱动轴对称推力矢量喷管逆运动学分析[J]. 航空动力学报, 2018, 33(1): 24-29. doi: 10.13224/j.cnki.jasp.2018.01.003
引用本文: 赵志刚, 李建鹏, 刘洋, 李维维. 三环驱动轴对称推力矢量喷管逆运动学分析[J]. 航空动力学报, 2018, 33(1): 24-29. doi: 10.13224/j.cnki.jasp.2018.01.003
Analysis on inverse kinematics of the three rings supporting and driving axialsymmetric vectoring exhaust nozzle[J]. Journal of Aerospace Power, 2018, 33(1): 24-29. doi: 10.13224/j.cnki.jasp.2018.01.003
Citation: Analysis on inverse kinematics of the three rings supporting and driving axialsymmetric vectoring exhaust nozzle[J]. Journal of Aerospace Power, 2018, 33(1): 24-29. doi: 10.13224/j.cnki.jasp.2018.01.003

三环驱动轴对称推力矢量喷管逆运动学分析

doi: 10.13224/j.cnki.jasp.2018.01.003

Analysis on inverse kinematics of the three rings supporting and driving axialsymmetric vectoring exhaust nozzle

  • 摘要: 针对某三环驱动轴对称推力矢量喷管,将喷管驱动结构分解为三个子模块,应用空间机构位置分析法、解析几何法、坐标转换法分别对上、中、下子模块进行分析,建立了完整的喷管驱动机构逆运动学模型,利用实体实验与仿真测试相结合的方法验证了喷管结构设计的合理性和所建模型用于喷管控制的有效性。所建模型准确率达到98%,为下一步喷管优化设计及控制器的研发提供了一定的理论基础。

     

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出版历程
  • 收稿日期:  2016-06-12
  • 刊出日期:  2018-01-28

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