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Hypersonic Periodic Cruise Trajectory Optimization Based on Flexible Use of Pseudo-spectral Method

机译:基于伪谱方法灵活使用的高超声速周期性巡航轨迹优化

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Periodical cruise can raise the fuel efficiency of hypersonic vehicle. Therefore, it is crucial to seek optimal characteristic parameters of periodical trajectory to establish a feasible guidance law in practice. In this paper, we employ the popular, mature and efficient nonlinear optimization scheme, pseudo-spectral method (PSM), to optimize the hypersonic periodic cruise in an innovative way by utilizing the symmetric property of periodic curve. Two optimization strategies, combined and entire ones, with artificial constraints for the sake of symmetry are provided and embedded within the PSM to obtain the optimal numerical solution. Then the parameters of specific periodic functions are fitted through nonlinear square method according to these numerical solutions. The numerical results of these two proposed methods and the optimal steady-state method are compared and investigated, demonstrating the effectiveness of the proposed methods.
机译:定期巡航可以提高高超音速飞行器的燃油效率。因此,寻求最优的轨迹轨迹特征参数在实践中建立可行的指导律至关重要。在本文中,我们采用流行,成熟且有效的非线性优化方案伪谱方法(PSM),通过利用周期曲线的对称性以创新的方式优化高超声速周期巡航。为了对称起见,提供了两种具有人工约束的组合优化和整体优化策略,并将其嵌入到PSM中以获得最佳数值解。然后根据这些数值解通过非线性平方方法拟合特定周期函数的参数。比较并研究了这两种方法和最优稳态方法的数值结果,证明了该方法的有效性。

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