Unique IRS (Inertial reference System), for safety critical applications, ITAR-FREE and based on high performance Fiber Optic Gyroscope (FOG)

G. Biancucci, R. Senatore, F. D'Angelo, A. Pizzarulli, M. Verola, E. Quatraro, D. Grifi, M. Perlmutter
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引用次数: 2

Abstract

ARGO 4000 is the outcome of three years of design and development effort carried out with the objective to realize the world smallest IRS (Inertial Reference System) certified by EASA with pending ETSO-c201, capable to provide high accuracy inertial navigation data in the most challenging environmental conditions applicable to fixed and rotary wing aircrafts and verified by means of the DO-160 standard qualification procedures. Such work has been partially financed by European Union H2020 SME innovation funds.ARGO 4000 architecture integrates a sensor block based on FOG’s (Fiber Optic Gyros) completely design and manufactured in-house using a proprietary technology, and on best-in-class Quartz accelerometers. The sensors are controlled by an extremely compact electronics compliant with DO-254, on which a DO-178C software executes the navigation algorithms to provide better than 1 NM/hr CEP (Circular Error Probable) and 0.05° heading accuracies. External GNSS and Air Data sensors can be interfaced through serial or ARINC-429 buses for aiding purposes. The architecture embeds a provision for extending the interface capabilities to further devices and communication standards (such as MIL-STD-1553) by means of a connecting bridge to an add-on-module, that can be customized with respect the specific platform-dependent integration requirements.ARGO 4000 development went through and extensive phase of simulation and experimental verification of many system aspects, fine tuning them to reach targeted performance and reliability.ARGO 4000 includes a sophisticated motion detection algorithm to improve the accuracy when aircraft is on ground and an IFA (In Flight Alignment) capability to manage emergency power switch off/switch on conditions during flight.ARGO 4000 is a dual-use, ITAR-free product, highly compact (4.1 kg, 3.1 liter) characterized by the best accuracy over weight and size ratio in the worldwide scenario.
独特的IRS(惯性参考系统),用于安全关键应用,ITAR-FREE和基于高性能光纤陀螺仪(FOG)
ARGO 4000是三年设计和开发工作的结果,目标是实现世界上最小的IRS(惯性参考系统),通过EASA认证,ETSO-c201待定,能够在最具挑战性的环境条件下提供高精度的惯性导航数据,适用于固定翼和旋翼飞机,并通过DO-160标准鉴定程序进行验证。这些工作部分由欧盟H2020中小企业创新基金资助。ARGO 4000架构集成了基于FOG(光纤陀螺仪)的传感器模块,采用专有技术完全设计和内部制造,以及一流的石英加速度计。传感器由一个非常紧凑的电子设备控制,符合DO-254标准,在DO-178C软件上执行导航算法,提供优于1 NM/hr CEP(圆形可能误差)和0.05°航向精度。外部GNSS和空气数据传感器可以通过串行或ARINC-429总线进行接口,以供辅助使用。该体系结构通过连接桥接到附加模块,将接口功能扩展到其他设备和通信标准(如MIL-STD-1553),可以根据特定的平台相关集成需求进行定制。ARGO 4000的开发经历了许多系统方面的模拟和实验验证的广泛阶段,对它们进行了微调,以达到目标性能和可靠性。ARGO 4000包括一个复杂的运动检测算法,以提高飞机在地面时的精度,以及在飞行过程中管理紧急电源开关/开关状态的IFA(飞行校准)能力。ARGO 4000是一种双重用途,无itar产品,高度紧凑(4.1公斤,3.1升),其特点是在全球范围内具有最佳的重量和尺寸比精度。
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