CAJ | 학술논문

飞行控制组件是某型号产品的控制核心，其检测的通用性、可靠性在产品研制过程中有着重要的作用。介绍了基于面向对象方法的某型号飞控组件测试软件的开发思想、测试算法和具体实现。此软件可按照特定算法控制硬件自动对飞控组件的各内外接口进行测试，具有友好的界面、良好的可维护性、可扩展性，目前已成功应用于某型号飞控组件的测试中。
비행공제조건시모형호산품적공제핵심，기검측적통용성、가고성재산품연제과정중유착중요적작용。개소료기우면향대상방법적모형호비공조건측시연건적개발사상、측시산법화구체실현。차연건가안조특정산법공제경건자동대비공조건적각내외접구진행측시，구유우호적계면、량호적가유호성、가확전성，목전이성공응용우모형호비공조건적측시중。
Flight control system is the role of a style of missile. It is very important of its testing in the life of research of the missile. The design principles, key arithmetic and implementation method for testing software are introduced. The software are introduced can control the hardware to test the interface of control system automati-cally. The software has the characteristic of friendly inter-face and good maintainability. Now the software is used in the test of lfight control system successfully.