iteration technique造句
例句与造句
- Axial iteration technique
轴向迭代法 - Here , we take the moser iteration technique and study the two kinds of problems submitted above
在本文中，我们利用moser迭代的技术分别对两类问题进行了讨论。 - During the solving process , the increment form can approximate the differential form and newton - raphson iteration techniques are introduced into the computation
求解实际中，可用增量形式代替微分形式，并且采用newton - raphson增量迭代法进行计算。 - In order to improve the efficiency , the fast far field approximation ( faffa ) and a novel local iteration technique based on dynamic coupling region controlling are applied to the original fipwa
为进一步提高求解效率,将快速远场近似与之混合;采用一种新型的动态控制耦合半径的局部迭代技术。 - By using cross - iteration technique and the schauder fixed point theorem , the existence theorem of travelling wave solutions of this system is established . and its application is made to the delay competitive system
针对反应项的不同单调性，引进交互迭代格式，利用schauder不动点定理建立了行波解的存在性定理，并将所得结论应用到时滞竞争系统。 - It's difficult to find iteration technique in a sentence. 用iteration technique造句挺难的
- Non - oscillatory and non - free - parameters dissipative ( nnd ) finite difference scheme ( a total variation diminishing scheme ) with second order accuracy was adopted to solve the fluid dynamic equations , a finite rate chemical reaction model was developed to calculate ingredient producing rate , and an adi over relaxation iteration technique was used to solve the electromagnetic discretized equations
采用二阶精度nnd格式求解流体力学方程组，采用有限速率化学反应模型计算组分生成率，采用交替方向隐式( adi )超松弛迭代法求解电磁场离散方程。 - Abstract : two computational techniques for inverse fight dynamics , namely derivation - iteration and integration - iteration techniques , are investigated . the application of inverse dynamics to determine control power requirements for post - stall maneuvering is researched , and a maneuvering flight trajectory based algorithm is provided , which lays a numerical foundation for simplifying design criteria for post - stall aircraft . with the model of inverse dynamics employed , a flight control mode for the outermost loop of the control system , named maneuver generator , is designed to follow desired complicated maneuvering flight trajectories . an example of rapid heading - reversal maneuver and other numerical simulations show the feasibility of the algorithm and the design idea
文摘:考察了求解输入类飞行逆动力学问题的微分-迭代与积分-迭代算法;探讨了利用逆动力学确定过失速机动操纵效能要求问题，这构成了进一步提出过失速机动飞机设计简化判据的数值基础;利用逆动力学设计机动发生模块进行飞控系统的最外环控制，以便跟踪期望的复杂机动轨迹.飞机最速反向示例及其它数值仿真结果表明设计思想与算法是可行的