宇航计测技术 ›› 2021, Vol. 41 ›› Issue (6): 15-22.doi: 10.12060/j.issn.1000-7202.2021.06.04

• 计量保障技术 • 上一篇    下一篇

深空探测运载火箭多弹道选择技术全系统测试研究

董余红,王建明,黄兵,刘秉,李茂,胡元威   

  1. 北京宇航系统工程研究所
  • 出版日期:2021-12-24 发布日期:2022-02-16
  • 作者简介:董余红(1979-),男,高级工程师,主要研究方向:运载火箭电气系统总体设计。

Research on the Whole System Test of Multiple Trajectory Selection Technology for Deep Space Exploration Launch Vehicle

Dong Yu-hong, Wang Jian-ming, Huang Bing, Liu Bing, Li Mao, Hu Yuan-wei   

  1. Beijing System Engineering Department
  • Online:2021-12-24 Published:2022-02-16

摘要: 针对深空探测任务发射机会少、发射窗口窄,若发射时间偏差较大则会造成探测器系统后续轨道修正过程中消耗较多推进剂的情况,本文提出在运载火箭测试发射过程中应用多弹道选择技术,给出多弹道选择技术的电气实现方案,以及多弹道选择技术的全系统测试方案。采用基于需求的系统测试技术,针对系统真实应用场景中可能发生的各种异常工况,设计了多个全系统测试用例,确保了多弹道选择技术在发射任务中的成功应用。

关键词: 深空探测, 多弹道选择, 全系统测试, 系统需求, 测试用例

Abstract: Specific to the situation that the deep space exploration task's fewer launch opportunities and narrower launch window, and that bigger launch time deviation can cause more propellant consumption during the deep space probe’s orbit correction process, this paper present the application of multiple trajectory selection technology in the launch vehicle’s testing and launching process, and then provide a electrical implementation scheme, and at last the whole system test scheme for multiple trajectory selection technology is also given. Adopting the system testing technology based on requirement, aiming at all kinds of abnormal working conditions that may occur in the real application scenarios of the system, a number of system-wide test cases were designed, that ensures the successful application of multiple trajectory selection technology in launch mission.

Key words: Deep space exploration, Multiple trajectory selection, The whole system test, System Requirement, Test Case

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