The design and development methods of aeroengine anti-surge control system are presented. Effects of heat disturbance parameters on the engine are analyzed during missile launch.
提出了航空发动机防喘控制系统设计和研制方法，分析了当战斗机发射导弹时热扰动参数对发动机的影响。
Agile development methods, which add program features iteratively, depend on refactoring as a technique to alter and extend a program's design.
敏捷开发方法采用迭代方式增加程序特性，因此需要依赖于重构技术来改变和扩展程序的设计。
And because agile project management embraces change and iterative development methods, it requires an efficient tool to make design and communication easy and fast.
同时，由于敏捷项目管理热衷于接受变更以及采纳迭代开发方法，因此需要一个有效的工具以更轻松和快捷地进行设计和交流。
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