Integrated GPS/Inertial Navigation for Aviation

机译：集成GPS /航空惯性导航

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This paper deals with an integrated navigation system for aircraft, which is based on satellite and inertial navigation. Aviation standards require a system integrity, which can only be met by using an appropriate integrity monitoring. Thus integrity monitoring is an essential feature of the integrated navigation system. The requirements and known approaches of integrity monitoring techniques are shown and suitable approaches are identified. These approaches are developed theoretically and evaluated based on simulations. Finally, the functions and performance of the developed navigation system will be demonstrated based on results from flight tests.

机译：本文研究了一种基于卫星和惯性导航的飞机综合导航系统。航空标准要求系统完整性，这只能通过使用适当的完整性监视来满足。因此，完整性监控是集成导航系统的基本功能。显示了完整性监控技术的要求和已知方法，并确定了合适的方法。这些方法是理论上开发的，并基于仿真进行了评估。最后，将基于飞行测试的结果演示开发的导航系统的功能和性能。

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来源
《Symposium gyro technology 2011 : Inertial sensors and systems 2011》|2011年|p.18.1-18.12|共12页
会议地点 Karlsruhe(DE);Karlsruhe(DE)
作者
T. Martin;
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Northrop Grumman LITEF GmbH Loerracher Str. 18 79115 Freiburg GERMANY Former Address Institute of Aerospace Systems Hermann-Blenk-Str. 23 38106 Braunschweig GERMANY;

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正文语种 eng
中图分类 U666.123;
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专利

1. An HSGPS, inertial and map-matching integrated portable vehicular navigation system for uninterrupted real-time vehicular navigation [J] . C. Basnayake, O. Mezentsev, G. Lachapelle, International Journal of Vehicle Information and Communication Systems . 2005,第1a2期

机译：用于不间断实时车辆导航的HSGPS，惯性和地图匹配的集成便携式车辆导航系统
2. A Modified Nonlinear Two-Filter Smoothing for High-Precision Airborne Integrated GPS and Inertial Navigation [J] . Gong Xiaolin, Zhang Jianxu, Fang Jiancheng Instrumentation and Measurement, IEEE Transactions on . 2015,第12期

机译：高精度机载集成GPS和惯性导航的改进非线性二滤波平滑
3. Sigma-point Kalman filtering for integrated GPS and inertial navigation [J] . Crassidis J.L. IEEE Transactions on Aerospace and Electronic Systems . 2006,第2期

机译：用于集成GPS和惯性导航的Sigma-point Kalman滤波
4. OEM4 Inertial: A Tightly Integrated Decentralised Inertial/GPS Navigation System [C] . Tom Ford, Janet Neumann, Pat Fenton, International Technical Meeting of the Satellite Division of the Institute of Navigation . 2001

机译：OEM4惯性：紧密综合的分散惯性/ GPS导航系统
5. Tightly integrated attitude determination methods for low-cost inertial navigation: Two-antenna GPS and GPS/magnetometer. [D] . Yang, Yunchun. 2001

机译：用于低成本惯性导航的紧密集成的姿态确定方法：两天线GPS和GPS /磁力计。
6. A Strap-Down Inertial Navigation/Spectrum Red-Shift/Star Sensor (SINS/SRS/SS) Autonomous Integrated System for Spacecraft Navigation [O] . Zhaohui Gao, Dejun Mu, Yongmin Zhong, 2018

机译：航天器导航的捷联惯性导航/光谱红移/恒星传感器（SINS / SRS / SS）自主集成系统
7. PC104 Based Low-cost Inertial/GPS Integrated Navigation Platform: Design and Experiments [O] . Di Li, René Jr. L 2015

机译：基于pC104的低成本惯性/ Gps组合导航平台：设计与实验
8. Miniature Inertial and Augmentation Sensors for Integrated Inertial/GPS Based Navigation Applications. [R] . Hopkins, R. E., Barbour, N. M., Gustafson, D. E., 2010

机译：用于基于惯性/ Gps的集成导航应用的微型惯性和增强传感器。

Integrated GPS/Inertial Navigation for Aviation

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