Any references found are resolved and the libraries are mapped into your program.
解决所有引用并把库映射到你的程序当中。
We designed the flight program for solid launch vehicles, resolved the control parameter of ascent trajectory with modified Newton iterative method, and deduced the iterative formula.
设计了固体运载火箭上升段飞行程序,应用修正牛顿迭代法求解上升段弹道控制参数,推导了迭代算法公式。
It may be resolved by the plane finite element computer program.
它适合于应用平面有限元法的计算程序求解。
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