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复合式共轴直升机过渡模式的操纵策略

王强 陈铭 徐冠峰

王强, 陈铭, 徐冠峰. 复合式共轴直升机过渡模式的操纵策略[J]. 航空动力学报, 2014, 29(2): 458-466. doi: 10.13224/j.cnki.jasp.2014.02.027
引用本文: 王强, 陈铭, 徐冠峰. 复合式共轴直升机过渡模式的操纵策略[J]. 航空动力学报, 2014, 29(2): 458-466. doi: 10.13224/j.cnki.jasp.2014.02.027
WANG Qiang, CHEN Ming, XU Guan-feng. Control strategy for compound coaxial helicopter under conversion mode[J]. Journal of Aerospace Power, 2014, 29(2): 458-466. doi: 10.13224/j.cnki.jasp.2014.02.027
Citation: WANG Qiang, CHEN Ming, XU Guan-feng. Control strategy for compound coaxial helicopter under conversion mode[J]. Journal of Aerospace Power, 2014, 29(2): 458-466. doi: 10.13224/j.cnki.jasp.2014.02.027

复合式共轴直升机过渡模式的操纵策略

doi: 10.13224/j.cnki.jasp.2014.02.027

Control strategy for compound coaxial helicopter under conversion mode

  • 摘要: 根据复合式共轴直升机的构型特点,建立了上/下旋翼、机翼、机身、全动平尾、垂尾(含方向舵)和螺旋桨的气动力模型,并在此基础上建立了过渡过程的配平方程.针对过渡飞行过程的操纵冗余问题,分别采用线性过渡和功率最小优化过渡两种过渡飞行方案,对复合式共轴直升机的过渡飞行过程的操纵策略进行了研究.以样例复合式共轴直升机为例,进行了过渡飞行模式下两种操纵策略的配平计算,并对两种过渡操纵策略下的需用功率、操纵量和姿态进行了对比.结果表明:所述两种过渡方案均能解决操纵冗余问题,并能合理给出过渡模式的操纵量和姿态.在操纵量变化的平稳度、飞行控制的难易程度和飞行品质方面,线性过渡方案更优.

     

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出版历程
  • 收稿日期:  2012-12-27
  • 刊出日期:  2014-02-28

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