该方案的安全性取决于求解因子分解问题与离散对数问题的计算难度。
The scheme's security is based on the computing difficulty of solving the Factorization Problem and the Discrete Logarithm Problem.
在机动边界点的求解上采用解析解和数值解对比的方法，降低了计算难度。
In the mobile boundary point by solving the analytical solution and numerical solution contrastive method, reduce the computational difficulty.
但它的作用机理比较复杂，气动设计计算难度较大，需要仔细地优选设计参数。
Nevertheless, it is complicated in mechanism and is difficult in the calculation of aero - dynamic design, and thus it is necessary that the design parameters should be optimized with carefulness.
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