当前和未来高g惯性测量单元的导航需求

IEEE PLANS 92 Position Location and Navigation Symposium Record Pub Date : 1992-03-23 DOI:10.1109/PLANS.1992.185832

A. Killen

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引用次数: 3

摘要

作者以先进动能导弹(ADKEM)惯性测量单元(IMU)性能要求为平台，讨论了各种误差源及其对ADKEM系统性能的影响，并指出了该技术未来可能的应用。特别注意的是ADKEM IMU误差预算。

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Navigational needs for current and future high-G inertial measurement units

The author uses the ADKEM (advanced kinetic energy missile) IMU (inertial measurement unit) performance requirements as a platform to discuss various error sources and their contribution to the ADKEM system performance and to indicate possible applications of this technology for the future. Particular attention is given to the ADKEM IMU error budget.<>

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IEEE PLANS 92 Position Location and Navigation Symposium Record

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