Abstract

Integrated Inertial Navigation System with camera-based system using LabVIEW Software

Highlights

  • To combine camera-based navigation and Inertial Navigation System (INS) in an integrated navigation system; through which we will obtain a system that unites: Microelectromechanical devices have created it attainable to manufacture tiny and light-weight guidance systems [1], [2]

  • An Inertial Measurement Unit (IMU) consists of an accelerometer, gyroscope, Pressure and magnetometer

  • The instruments pivotal to the actual pretense of this project have been selected such that they provide high accuracy while not amounting to the budget being overshot

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Summary

INTRODUCTION

To combine camera-based navigation and INS in an integrated navigation system; through which we will obtain a system that unites: Microelectromechanical devices have created it attainable to manufacture tiny and light-weight guidance systems [1], [2] These advances have widened the range of possible applications to incorporate areas like human and animal motion capture. Inertial Navigation System (INS) is a computer based selfcontained system that will provide aircraft’s geographic information in terms of latitude and longitude with aircraft speed, heading and tracking information. It can provide wind velocity and direction if we use True Air Speed (TAS) as an input value. Some of their features are: It supports two-way telemetry and in-flight command using the powerful MAVlink Protocol

METHODOLOGY
RESULTS AND DISCUSSION
CONCLUSION AND FUTURE SCOPE
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