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该文建立了求解折叠翼火箭满足散布极小化和飞行稳定性要求的最佳尾翼延时张开时问的数学模型和计算方法.实际算例说明了本方法的具体应用,且得到了与文献[1]形状相同的曲线.
In this paper, a mathematic model and calculation method are proposed to solve the optimal delay time when the folded-wing rocket satisfies the requirements of scatter minimization and flight stability.The practical examples illustrate the specific application of this method, 1] The same shape of the curve.