CAJ | 학술논문

传统导弹发控系统检测功能单一,缺乏定量分析能力和故障诊断手段;采用"测试发控"一体化技术,利用虚拟仪器"软件就是仪器"的优点,在传统射检发控功能的基础上集成了动态检测功能和快速故障诊断功能;阐述了系统设计的基本方法和实现过程,包括设计思想、总体方案、信号适配电路设计、软件计数算法和动态测试技术的实现等内容;实践表明,该系统有效提升了导弹发控系统的技术水平和层次,为导弹发射成功提供了可靠保障.
전통도탄발공계통검측공능단일,결핍정량분석능력화고장진단수단;채용"측시발공"일체화기술,이용허의의기"연건취시의기"적우점,재전통사검발공공능적기출상집성료동태검측공능화쾌속고장진단공능;천술료계통설계적기본방법화실현과정,포괄설계사상、총체방안、신호괄배전로설계、연건계수산법화동태측시기술적실현등내용;실천표명,해계통유효제승료도탄발공계통적기술수평화층차,위도탄발사성공제공료가고보장.
In the traditional launch control system detection weaknesses of single detection function, short of quantitative analysis and fault diagnosis capability. Adopting incorporated technology of test &-launch Control and making use of the Ⅵ' s characteristic that "software is instruments", missile dynamic test function and quick diagnoses function are integrated on the foundation of traditional launch control system. This dissertation elaborates the means and realization of the system, such as design ideas, general project, signal adaption circuit,software realization means of pulse cluster counter and realization of misile dynamic test. It is shown that the system improves the technical level of missile launch control system and provides dependable safeguard for launch successfully.