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Attitude and Heading Reference System for Aerospace Application

Kirthana B1 , Madhushree K2 , Madhushree M S3 , Megha P H4 , Dhanraj S5

Section:Research Paper, Product Type: Journal Paper
Volume-07 , Issue-15 , Page no. 73-77, May-2019

CrossRef-DOI:   https://doi.org/10.26438/ijcse/v7si15.7377

Online published on May 16, 2019

Copyright © Kirthana B, Madhushree K, Madhushree M S, Megha P H, Dhanraj S . 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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IEEE Style Citation: Kirthana B, Madhushree K, Madhushree M S, Megha P H, Dhanraj S, “Attitude and Heading Reference System for Aerospace Application,” International Journal of Computer Sciences and Engineering, Vol.07, Issue.15, pp.73-77, 2019.

MLA Style Citation: Kirthana B, Madhushree K, Madhushree M S, Megha P H, Dhanraj S "Attitude and Heading Reference System for Aerospace Application." International Journal of Computer Sciences and Engineering 07.15 (2019): 73-77.

APA Style Citation: Kirthana B, Madhushree K, Madhushree M S, Megha P H, Dhanraj S, (2019). Attitude and Heading Reference System for Aerospace Application. International Journal of Computer Sciences and Engineering, 07(15), 73-77.

BibTex Style Citation:
@article{B_2019,
author = {Kirthana B, Madhushree K, Madhushree M S, Megha P H, Dhanraj S},
title = {Attitude and Heading Reference System for Aerospace Application},
journal = {International Journal of Computer Sciences and Engineering},
issue_date = {5 2019},
volume = {07},
Issue = {15},
month = {5},
year = {2019},
issn = {2347-2693},
pages = {73-77},
url = {https://www.ijcseonline.org/full_spl_paper_view.php?paper_id=1204},
doi = {https://doi.org/10.26438/ijcse/v7i15.7377}
publisher = {IJCSE, Indore, INDIA},
}

RIS Style Citation:
TY - JOUR
DO = {https://doi.org/10.26438/ijcse/v7i15.7377}
UR - https://www.ijcseonline.org/full_spl_paper_view.php?paper_id=1204
TI - Attitude and Heading Reference System for Aerospace Application
T2 - International Journal of Computer Sciences and Engineering
AU - Kirthana B, Madhushree K, Madhushree M S, Megha P H, Dhanraj S
PY - 2019
DA - 2019/05/16
PB - IJCSE, Indore, INDIA
SP - 73-77
IS - 15
VL - 07
SN - 2347-2693
ER -

           

Abstract

Many experiments have been conducted for attitude estimation with low cost micro electro-mechanical system (MEMS), even though it was of low cost and less weight it causes certain noise and errors over time. The main objective of the paper is to introduce accelerometer portion of basic attitude and heading reference system for aerospace application using Internet of Things (IoT) which can be used to find the optimal weight value such error of the Attitude and Heading Reference (AHRS) is minimised. The proposed system also assures the body rate by using 2 axis gyro and it provides distance rate measurement and angular rotation. This system consumes low power and easy to handle.

Key-Words / Index Term

ArdiunoUno, Accelerometer, Gyroscope, Magnetometer

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