面向测控的运载火箭仿真设计与实现  

Design and Realization of TT&C-Oriented Simulation of Launch Vehicle

作　　者：杨永安[1] 冯祖仁[1] 杜小宁[2] 王波[2] 张宏伟[2] 

机构地区：[1]西安交通大学,西安710049 [2]西安卫星测控中心,西安710043

出　　处：《系统仿真学报》2004年第11期2507-2510,共4页Journal of System Simulation

基　　金：运载火箭遥外测平台仿真系统

摘　　要：随着航天测控系统任务日益增多、周期缩短、技术要求提高等现实,如何确保每次实战任务地面火箭遥测设备和测控软件的正常运行,火箭外测和遥测数据处理快速准确,对航天测控系统而言尤为重要和迫切,而构建面向测控的运载火箭仿真是解决此问题的重要手段之一。本文首先介绍了面向测控的运载火箭仿真的功能需求和系统组成;其次提出了面向测控的运载火箭仿真系统设计方案以及测试方法;最后总结了面向测控的运载火箭仿真的应用情况和发展方向。With the rapid increase of the space tracking, telemetry and control (TTC) system mission, the mission period becomes shorter and the technical requirements are higher. Therefore, two problems must be solved in the space TTC system task: one is to ensure the ground launch vehicle telemetry equipments and TTC software work properly, and the other is to ensure the launch vehicle telemetry date and trajectory data are processed quickly and accuracy. One of the important methods to solve the problems is the TTC-Oriented Launching Vehicle Simulation (TTCOLVS), which is studied in the paper. Firstly, the function demands and system composition of TTCOLVS are presented. Secondly, the design scheme and test methods of TTCOLVS are brought forward. Finally, the application instances and development tendency of TTCOLVS are summarized.

关 键 词：面向对象 航天测控系统 仿真技术 运载火箭 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]