首页> 外文会议>Saint Petersburg International Conference on Integrated Navigation Systems >PERFECTION OF THE ONBOARD SOFTWARE FOR THE FIRST INTEGRATED INS/ (GLONASS GPS) SYSTEM OF NAVIGATION AND ATTITUDE OF THE LAUNCHER. SYSTEM FLIGHT TESTS OUTCOMES
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PERFECTION OF THE ONBOARD SOFTWARE FOR THE FIRST INTEGRATED INS/ (GLONASS GPS) SYSTEM OF NAVIGATION AND ATTITUDE OF THE LAUNCHER. SYSTEM FLIGHT TESTS OUTCOMES

机译:用于发射器导航和态度的第一个综合INS /(GLONASS和GPS)系统的船上软件的完善。系统飞行测试结果

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摘要

Formation principles of the first inertia! satellite-aided navigation and attitude system onboard software for a launch vehicle is under consideration. Onboard software evolution from launch to launch as well as Us complication and expansion is shown. Computational procedures, forming a kernel of integrated system unified technology for objects with increased requirements to informational reliability, are presented. The purpose of the technology is to protect navigational trajectory and guidance loop from the GLONASS/GPS receiver false data. Performance and accuracy of the system are analyzed on upper stage (US) "Fregat "flight tests. Ways for the inertial and satellite systems integration improvement and adaptation for modern space technology are discussed.
机译:第一个惯性的形成原则!正在考虑用于发射车辆的卫星辅助导航和态度系统。从发射到启动以及我们的复杂和扩展,从船上软件演进。展示了计算过程,为具有增加的信息可靠性的对象形成集成系统统一技术的内核。该技术的目的是保护来自Glonass / GPS接收器错误数据的导航轨迹和引导循环。在上阶段(US)“Fregat”飞行试验中分析了系统的性能和准确性。讨论了惯性和卫星系统集成改进和现代空间技术适应的方式。

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