1) prediction-verification
预测-校验
1.
A novel least squares algorithm based on anti-WKB method and linear segment interpolation,which is called prediction-verification method, is proposed.
提出一种基于反WKB法与分段线性插值的最小二乘拟合方法(即预测-校验方法)来确定离子交换玻璃波导的横向折射率分布,它将反WKB法与分段线性插值所计算出的结果作为近似值(预测),然后进行最小二乘拟合(校验),并与基于反WKB的分段线性插值方法进行比较。
2) prior checking
预先校验
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。
5) Detection and verification
检测校验
6) check test
校验测试
1.
Taking the check test of CDMA mobile phone and different characteristic test of GSM mobile phone as an example,the effectiveness and veractiy of the system are validated.
以CDMA手机的校验测试和GSM手机各种特征参数测试为例,验证了该测试系统的有效性和准确性。
补充资料：发育进度预测法(见发生期预测)
发育进度预测法(见发生期预测)
发育进度预测法见发生期预测。
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