探空火箭有效载荷集成测试系统设计与实现

摘要

Scheme for integrated test system is put forward, the test system hardware platform and software architecture are introduced, the method for their design and implementation is analyzed and elaborated. Successful application demonstrates that the system meets all the test requirements of sounding rocket payloads, has good generality and scalability, and provides some reference for the test and verification of sounding rockets, as well as serialization, generalization and standardization of related test facilities.%介绍了应用于探空火箭有效载荷集成测试的系统设计方案,描述了测试系统硬件平台和软件架构,对设计与实现方法进行了分析和阐述.探空火箭成功发射的经验表明,系统满足探空火箭有效载荷的集成测试需求,具有较好的通用性及可扩展性,从而为探空火箭型号的系统测试与验证以及相关测试设备的系列化、通用化和标准化提供了一定的借鉴.