基于地面软件自动生成控制诸元的方法研究

Research on the Automatic Generation of Control System Parameters Based on the Ground Software

摘要:

针对目前运载火箭诸元文件研制流程繁琐、质量过程控制存在风险等问题，提出一种由地面软件自动生成飞行诸元、瞄准诸元的方法。鉴于某型号火箭发射地点固定的特点，将不随飞行任务变化的标准诸元固化在地面测控计算机本地，由地面软件对标准诸元的指定飞行参数完成合理性判别与装订，实现与飞行任务匹配的飞行诸元自动生成；利用箭载计算机与地面测控计算机之间瞄准数据交互，由地面软件完成自瞄准数据实时监测、瞄准参数冗余校验及自瞄准诸元自动生成等功能。通过工程实践验证了控制系统诸元文件生成过程实现简单，生成结果准确，相比传统研制流程，有效缩短研制周期，满足了运载火箭高密度发射要求。

Abstract:

Aiming at the problems of complex development process and risk in quality process control of launch vehicle, an innovative method is proposed for the automatic generation of flight firing data and aiming data by ground software. In accordance with the characteristic that the launch site of a rocket is fixed, the rationality of the specified flight parameters for standard elements is evaluated and calibrated by ground software, and the flight firing data that matching the flight mission is generated automatically. By using the aiming data interaction between the on-board computer and the ground measurement and control computer, ground software completes the real-time monitoring of the self-aiming data, the redundancy check of the aiming parameters and the automatic generation of the self-aiming data. Many engineering practices have verified that the generation process of the control system parameters is simple, and the generated results are accurate. Compared with the traditional development process, it effectively shortens the development cycle and meets the requirements of high - density launches of launch vehicle.