1) Adams-Moulton predictor-corrector method
亚当姆预测-校正系统
1.
Considering phase and intensity distribution changed when Gaussian beam transmitted through the Kerr media,based on the Adams-Moulton predictor-corrector method and the Huygens-Fresnel diffraction,near-field and far-field of the light intensity distribution are investigated when a Gaussian beam transmitted through a Kerr medium,respectively.
以亚当姆预测-校正系统数值计算方法为基础,在同时考虑光束通过克尔介质后的相位和光束线型变化的情况下,利用惠更斯-菲涅尔衍射积分公式,对高斯光束通过克尔介质后的近场和远场的横向光强分布进行了研究。
2) eulermethod
预估-校正系统
3) predictor-corrector
预测校正
1.
Reentry guidance law design for RLV based on predictor-corrector method
基于预测校正方法的RLV再入制导律设计
2.
This paper discusses the value of central parameter effecting on the convergence of the primal-dual interior point algorithm,based on which a predictor-corrector technology is adopted to enhance.
在此基础上引入预测校正环节,该方法能很好地协调解的最优性和可行性之间的关系,改善了算法的收敛性;采用IEEE14节点标准测试系统进行实时电价计算,对仿真结果的分析表明了相应不等式约束的Lagrangian乘子的值代表系统运行安全费用,预测校正法迭代次数少,收敛性好。
3.
The primal-dual interior point algorithm is applied in global optimization on the basis ofnon-linear programming model for voltage-reactive power optimization,based on which a predictor-corrector technology is adopted to enhance the convergence by coordinating the optimality and feasibility.
以电力系统中电压无功优化的非线性规划模型为基础,采用原对偶内点算法进行全局寻优;并在此基础上提出了一种预测校正方法,该方法通过协调解的最优性及可行性之间的关系提高算法的收敛性。
4) predictor-corrector
预测-校正
1.
The predictor-corrector reentry guidance algorithm for reusable launch vehicles was studied.
研究了可重复使用运载器的预测-校正再入制导方案。
2.
For the guidance law design problem of lunar spacecraft reentry at the second cosmic velocity,a predictor-corrector guidance method is adopted.
针对以第二宇宙速度返回的探月飞船再入制导律设计问题,采用一种数值预测-校正的预测制导法,分析了飞船配平攻角的飞行特性,建立了再入三自由度运动方程,进而详细介绍了预测-校正及其纵向、横向制导律的基本原理。
补充资料：飞机校靶(见飞机武器系统校正)
飞机校靶(见飞机武器系统校正)
aircraft boresighting
feiii iiaoba飞机校靶(airerart boresighting)见飞机武器系统校正。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条