张忠峰, 高云峰, 宝音贺西. 高超声速飞行器周期巡航条件的确定[J]. 力学与实践, 2009, 31(1): 16-19. DOI: 10.6052/1000-0879-2008-026
引用本文: 张忠峰, 高云峰, 宝音贺西. 高超声速飞行器周期巡航条件的确定[J]. 力学与实践, 2009, 31(1): 16-19. DOI: 10.6052/1000-0879-2008-026
DETERMINATION OF PERIODIC CRUISE CONDITION OF HYPERSONIC VEHICLE[J]. MECHANICS IN ENGINEERING, 2009, 31(1): 16-19. DOI: 10.6052/1000-0879-2008-026
Citation: DETERMINATION OF PERIODIC CRUISE CONDITION OF HYPERSONIC VEHICLE[J]. MECHANICS IN ENGINEERING, 2009, 31(1): 16-19. DOI: 10.6052/1000-0879-2008-026

高超声速飞行器周期巡航条件的确定

DETERMINATION OF PERIODIC CRUISE CONDITION OF HYPERSONIC VEHICLE

  • 摘要: 针对不同已知条件,分别用Newton-Raphson迭代法和遗传算法确定了高超声速飞行器周期巡航的条件. 并且用胞映射法计算得到周期巡航不动点的吸引域. 结果表明,只要满足特定条件,高超声速飞行器就可实现周期巡航,且巡航初始值可在较大的范围内进行选择.

     

    Abstract: According to different available conditions, periodiccruise conditions of a hypersonic vehicle are determined by Newton-Raphson'siteration and Genetic Algorithm. The attraction region of fixed pointsof the periodic cruise is obtained by a cell-to-cell mapping method. The resultsindicate that the hypersonic vehicle can cruise periodically under certainconditions and initial values of the periodic cruise can be selected in a widerange.

     

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