首页> 外文会议>55th International Astronautical Congress 2004 vol.9 >MARS EXPLORATION ROVER MISSION: ENTRY, DESCENT, AND LANDING SYSTEM VALIDATION
【24h】

MARS EXPLORATION ROVER MISSION: ENTRY, DESCENT, AND LANDING SYSTEM VALIDATION

机译:火星探测车任务:进入,下降和着陆系统验证

获取原文
获取原文并翻译 | 示例

摘要

System validation for a Mars entry, descent, and landing system is not simply a demonstration that the electrical system functions in the associated environments. The function of this system is its interaction with the atmospheric and surface environment. Thus, in addition to traditional test-bed, hardware-in-the-loop, testing, a validation program that confirms the environmental interaction is required. Unfortunately, it is not possible to conduct a meaningful end-to-end test of a Mars landing system on Earth. The validation plan must be constructed from an interconnected combination of simulation, analysis and test. For the Mars Exploration Rover mission, this combination of activities and the logic of how they combined to the system's validation was explicitly stated, reviewed, and tracked as part of the development plan.
机译:火星进入,下降和着陆系统的系统验证不仅仅是电气系统在相关环境中起作用的证明。该系统的功能是其与大气和地面环境的相互作用。因此,除了传统的测试台,硬件在环测试之外,还需要用于确认环境相互作用的验证程序。不幸的是,不可能对地球上的火星着陆系统进行有意义的端到端测试。验证计划必须由仿真,分析和测试的相互结合构成。对于火星探索漫游者任务,这种活动的组合以及它们如何与系统验证相结合的逻辑已明确说明,审查和跟踪,这是开发计划的一部分。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号