English translation for "一致性约束"
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- consistency constraints
Related Translations:
一致: fit; showing no difference; identical; unanimous; consistent; in accordance with; in accord; agreed; in keeping with; interconsistency; coincide; uniform 短语和例子一致决定 unanimous decision; 一致表决 拟一致: quasi steadyquasisteadyquasiuniform 一致熔融: congruent meltingcongruentmelting 一致同意: accord and satisfsctionconsensusunanimous agreementunanimous co entunanimous consent 一致角速度: uniform angular velocity 祖先一致: ancestral identities 磁约束激光器: magnetically confined laser
- Example Sentences:
| 1. | 3 . a stereo matching algorithm based on ordering coherence constraint is presented
3 .提出一种基于顺序一致性约束的立体匹配算法。 | | 2. | The consistency constraints provide a way to decouple the disciplines and make the parallel subsystem optimization possible
通过引进一致性约束条件,实现学科之间的解耦和并行优化。 | | 3. | Based on the compatibility constrained optimization and the collaborative optimization , this thesis proposes a two - level optimization approach for integrated aerodynamic / structural design of wings
本文借鉴多学科设计优化算法中的一致性约束算法和协同优化算法,提出了面向飞机气动/结构一体化设计的二级优化方法。 | | 4. | Collaborative optimization ( co ) , originated from the compatibility constrained optimizaiton ( cco ) , is a bi - level optimization algorithm based on system decomposition and coordination
协作优化算法（ collaborativeoptimizaiton ，简称co ）是在一致性约束优化算法（ compatibilityconstrainedoptimization ，简称cco ）的基础上发展起来的，基于分解和协调的一种双层优化算法。 | | 5. | In this approach , design tasks are decomposed into a system - level optimization and subsystem - level optimizations . the task of each subsystem optimization is to find the local variables to minimize or maximize objectives , subject to its local design constraints . the task of the system - level optimization is to find global ( or shared ) and auxiliary variables to optimize the system performances , and satisfy the consistency constraints
这种方法将优化流程分为系统级优化和单学科优化两个层次:系统级优化的任务是通过调整共享设计变量和辅助设计变量,在满足一致性约束条件下,使系统目标最优;子系统的任务是调整局部设计变量,在满足本学科的设计要求条件下,使子系统的目标最优。 | | 6. | Abstract : a new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
文摘:探讨了一种新的设计指标最优分配方法- -协同分配法,用于处理飞机顶层设计中的大规模设计指标最优分配问题.分析了飞机顶层设计中的设计指标最优分配特征,据此给出了协同法的原理并建立了数学模型.协同法按设计指标分配关系将最优分配问题分解为主系统优化和子系统优化,主优化对子系统设计指标进行最优分配,子优化以最小化分配设计指标值与期望设计指标值之间的差异为目标,进行子系统最优设计,或对底层元件(如飞机翼梁、翼肋和翼盒等)进行设计指标最优分配,并把最优解信息反馈给主优化.主优化通过子优化最优解信息构成的一致性约束协调分配量,提高系统整体性能,并重新给出分配方案.主系统与子系统反复协调,直到得到设计指标最优分配方案.两层可靠度指标分配算例初步验证了本文方法的正确性与可行性,三层可靠度指标分配算例证明了本文方法的有效性.最后,以重量指标分配为例,简要叙述了针对飞机顶层设计中设计指标协同分配的数学模型和求解思路 | | 7. | A new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
探讨了一种新的设计指标最优分配方法- -协同分配法,用于处理飞机顶层设计中的大规模设计指标最优分配问题.分析了飞机顶层设计中的设计指标最优分配特征,据此给出了协同法的原理并建立了数学模型.协同法按设计指标分配关系将最优分配问题分解为主系统优化和子系统优化,主优化对子系统设计指标进行最优分配,子优化以最小化分配设计指标值与期望设计指标值之间的差异为目标,进行子系统最优设计,或对底层元件(如飞机翼梁、翼肋和翼盒等)进行设计指标最优分配,并把最优解信息反馈给主优化.主优化通过子优化最优解信息构成的一致性约束协调分配量,提高系统整体性能,并重新给出分配方案.主系统与子系统反复协调,直到得到设计指标最优分配方案.两层可靠度指标分配算例初步验证了本文方法的正确性与可行性,三层可靠度指标分配算例证明了本文方法的有效性.最后,以重量指标分配为例,简要叙述了针对飞机顶层设计中设计指标协同分配的数学模型和求解思路 | | 8. | The rtsql includes extensions that specify : temporal constraints on data , timing constraints on execution , bounds on use of system resources for predictability , and flexible transaction structure that relaxes traditional acid transaction properties to better support real - time requirements . a framework for the implementation of rtsql is provided in this paper
对sql92的扩展主要体现在:数据时态一致性约束的表达和检测，事务执行时态一致性约束的表达和检测，为提高事务执行的可预测性而对其使用的系统资源进行限制性说明，以及为了更好适应实时要求而提供灵活acid特性的事务结构说明。 | | 9. | Xrdbm improves xml - dbms at following aspects : the consistency maintaining method during transforming semi - strctured data model into relation model , the maintenance of xml document and the problem of different subelements with the same name , etc . based on xrdbm , the author proposes an algorithm of xml publishing to deal with the input sql statements and generate valid xml document for the certain dtd automatically , named valid xml generating from sql ( vxg - sql )
Xrdbm对xml - dbms进行了如下改进和完善，包括dtd生成关系模式中常见的子元素重名、 xml文档在关系数据库中的维护、关系模式和半结构化模型之间映射的一致性维护方法等。在xrdbm基础之上，作者设计并实现了根据sql语句自动生成符合dtd 、满足一致性约束的xml文档的算法vxg - sql 。 | | 10. | Interval frame classification is proposed . in this thought , features extract and classification are treated at interval frames instead of each frame , which debases time complexity of classification algorithm . and the methods of using temporal consistency and scene - dependent features are described
提出隔帧分类的思想,将每帧都进行的特征提取与分类处理改为隔帧处理,降低了分类算法的时间复杂度,并描述了利用时间一致性约束和场景相关特征提高分类效率的方法。 |
- Similar Words：
- "一致性信息" English translation, "一致性选择子句" English translation, "一致性与测试" English translation, "一致性语言" English translation, "一致性原则" English translation, "一致性证书" English translation, "一致性指标" English translation, "一致性指数" English translation, "一致性质" English translation, "一致性质量" English translation
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