The Design of INS under PBN

Ming Qiang Chen

doi:10.4028/www.scientific.net/AMM.336-338.1028

Paper Titles

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“3G Network” Platform-Based Design for Smart Car Remote Telemetry and Control
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Structural Analysis of a Grinding Machine with Linear Motion Guide Applied
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The Temperature Control System Design of Microchip Level PCR Instrument Based on SOPC
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The Design of INS under PBN
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Research Status and Key Technology of Portable Open-Loop Insulin Pump
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Research on Variable Steering Ratio of Vehicle Steer-by-Wire System Based on Joystick
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Exploration of Magnetically Controlled Shape Memory Alloy Vibration Energy Harvestor
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Joint Stiffness Identification and Flexibility Compensation of Articulated Industrial Robot
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 336-338The Design of INS under PBN

The Design of INS under PBN

Abstract:

The Global Positioning System (GPS) has been approved for a limited number of applications in civil aviation because it is not highly available for meeting safety-of life levels of integrity, which require timely alert if the system is unreliable for navigation under the environment of Performance Based on Navigation (PBN). This paper presents an analysis about principle of an inertial navigation system (INS) and design an new mechanical architecture of INS in terms of increased availability of GPS for civil aviation. This new mechanical architecture has a good mechanical properties in mechanical engineering of civil aviation.