Design and Development of a Multifunctional Flight Display System

Wen Chi Lu; Ming Wei Wang

doi:10.4028/www.scientific.net/AMM.664.293

Paper Titles

Optical Computer Mouse Referenced Calibration of an Inertial Measurement Unit for Use in Unmanned Underwater Vehicles
p.274

A New Dielectric Elastomer Sensor Based on Cantilever Beam Structure with Constant Strength
p.279

Numerical Analysis of the Failure Modes for the Circular Dielectric Elastomer Actuator
p.284

Study of On-Line Detection of Voltage Transient Disturbance Based on DSP and Wavelet
p.288

Design and Development of a Multifunctional Flight Display System
p.293

Attitude Measurement Low Frequency Error Identification and Compensation for Star Tracker with Gyros
p.298

Measurement of Polycrystalline Diamond Craters in Electrical Discharge Machining
p.304

Comparative Research of 240-Coil Permanent Magnetic Brushless Motor with or without Potting Compound
p.313

Application Analysis of Expanded Conductor in 1000kV UHV Double-Circuit Line
p.318

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 664Design and Development of a Multifunctional Flight...

Design and Development of a Multifunctional Flight Display System

Abstract:

The paper presents the development of a multifunctional flight display system for light-sport aircraft flying. The requirements and design of the system is discussed. It is mainly designed as a backup system for flying rather than a certified flight instrument. An ARM-core embedded system is chosen as the development platform with Linux operation system. The system basically takes advantage of 3-D positioning information from GPS which has been widely used on general aviation aircraft. Its diverse interfaces provide system redundancy with wired or wireless connection to external sensor systems for aircraft attitude, pressure height, and magnetic heading. The proposed flight display system has been developed and running over the embedded system.