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首页> 外文会议>UAVs Eighteenth International Conference Mar 31-Apr 2, 2003 Bristol, United Kingdom >SiNAV~(TM) - Integrated MEMS/GPS Navigation System
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SiNAV~(TM) - Integrated MEMS/GPS Navigation System

机译：SiNAV〜（TM）-集成MEMS / GPS导航系统

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摘要

This paper describes the development of SiNAV~(TM)-BAE SYSTEMS' integrated MEMS-based inertial sensor/GPS navigation systems. Underlying MEMS capability is outlined, and the significance of this technology as a component in low-cost, miniature and gun-hard navigation systems is described. A series of BAE SYSTEMS' integrated inertial sensor/GPS systems are described, in accordance with the SiNAV? development routemap. This commences with first-generation, loosely-coupled systems, to higher performance, closely-coupled systems being developed today for tactical missiles and UAVs, culminating in deeply-integrated, gun-hard high anti-jam systems for guided projectiles. All phases of SiNAV~(TM) employ a modular and flexible Kalman filter. This, in addition to the potential for exploiting this flexibility by employing alternative aiding sources, is described.
机译：本文介绍了SiNAV〜（TM）-BAE SYSTEMS集成的基于MEMS的惯性传感器/ GPS导航系统的开发。概述了MEMS的基本功能，并描述了该技术作为低成本，微型且具有枪法性的导航系统中的组件的重要性。根据SiNAV ?，描述了一系列BAE SYSTEMS的集成惯性传感器/ GPS系统。开发路线图。这始于第一代松耦合系统，再到今天为战术导弹和无人机开发的高性能，紧密耦合系统，最终形成了用于炮弹的深度集成，高炮制高抗干扰系统。 SiNAV〜（TM）的所有阶段均采用模块化且灵活的卡尔曼滤波器。除了通过采用替代辅助源来利用这种灵活性的潜力外，还对此进行了描述。

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