Integrated Micro-Electro-Mechanical Systems with Global Position System for Attitude Measurements of Aerial Vehicles

M. Raja¹ , Abishek Marwaha² , Devison J Kochuveettil³ , Bathula Narender⁴ , Abhishek Sharma⁵

Section:Research Paper, Product Type: Journal-Paper
Vol.6 , Issue.8 , pp.14-17, Aug-2020

Online published on Aug 31, 2020

Copyright © M. Raja, Abishek Marwaha, Devison J Kochuveettil, Bathula Narender, Abhishek Sharma . This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
 

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Abstract :
To design a low-cost accurate navigation system using Global position system (GPS) and Micro Electro Mechanical system (MEMS). This paper to implement the algorithms an accurate navigation system with help of Integration of MEMS and GPS using Kalman filter. Integration of these two different navigation system gives the best estimation of the attitude of the aircraft excluding almost all the errors. By Utilization of MPU6050 the results by taking the most exact of the results given by GPS and MEMS. The scope of the experiments is to design and manufacture a model which is accurate and at the same time cost efficient. We intend on making a navigation system that estimates the orientation and position, and rather than using expensive and delicate hardware, we are trying to compensate the above mentioned difficulties with cost efficient and easy and efficient techniques

Key-Words / Index Term :
Global position system, Micro Electro Mechanical system, MPU6050, Euler angles

References :
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