运载火箭地面一体化测发控系统设计

Design of Integrated Ground Test Launch and Control System of Launch Vehicle

摘要:

现役运载火箭各分系统的测发控系统各自独立，存在资源浪费，兼容性差、信息传递低效等问题。随着测控技术发展和火箭电气系统需求牵引，新一代运载火箭地面测试、发射与控制在通用化、集成化、智能化等方面提出了更高的要求。通过梳理一体化设计的功能，提出一种运载火箭地面测发控系统的体系架构，整合传统运载火箭控制、测量、总控网等分系统的测发控共性需求，在统一供配电、有线测控、无线调解调、数据处理与分析4个功能层面进行设计，包括系统组成、交互关系、重要单机（软件）的设计及其关键技术应用。该设计在某型号完成了原理性试验和关键技术验证，结果表明系统通用性强、集成度高、信息架构合理高效，能够在确保可靠性安全性的情况下，简化操作、提高效率、降低成本。

Abstract:

The test launch and control system of active launch vehicle is independent, there are some problems such as waste of resources, poor compatibility and low efficiency of information transmission. With the development of test and control technology and the requirement of launch vehicles, the ground test launch and control of new launch vehicles have put forward higher requirements in the aspects of generalization, integration and intelligentization. By analyzing the function of the integrated design, it puts forward a kind of ground test launch and control system architecture, effectively integrates the common requirements of subsystems of traditional launch vehicle. The Design is carried out at four functional levels of the unity power supply, cable test and control, wireless mediation, data process and analysis, including the design and key technologies of the system composition, interaction, important equipment and software. In a certain model, the fundamental and key technology test show that the system has strong universality, high level of integration, efficient information architecture, it can simplify operation, improve efficiency and reduce cost while ensuring reliability and safety.