This paper is published in Volume-4, Issue-3, 2018
Area
Intra-Satellite Communication
Author
Vrushank Sastry, Veeraiah Yarasi, Sreekar Mayakuntla, Chaluvaraju P P
Org/Univ
School of Engineering and Technology Jain University (SET JU), Bengaluru, Karnataka, India
Pub. Date
19 May, 2018
Paper ID
V4I3-1455
Publisher
Keywords
Intra-satellite communication, Lpc2148, Arduino Mega2560, Wireless communication, Attitude and orbit control system (AOCS), Bluetooth module HC-05, Sensors, and actuators

Citationsacebook

IEEE
Vrushank Sastry, Veeraiah Yarasi, Sreekar Mayakuntla, Chaluvaraju P P. Multi-channel wireless signal transmission system for intra-satellite communication, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.

APA
Vrushank Sastry, Veeraiah Yarasi, Sreekar Mayakuntla, Chaluvaraju P P (2018). Multi-channel wireless signal transmission system for intra-satellite communication. International Journal of Advance Research, Ideas and Innovations in Technology, 4(3) www.IJARIIT.com.

MLA
Vrushank Sastry, Veeraiah Yarasi, Sreekar Mayakuntla, Chaluvaraju P P. "Multi-channel wireless signal transmission system for intra-satellite communication." International Journal of Advance Research, Ideas and Innovations in Technology 4.3 (2018). www.IJARIIT.com.

Abstract

An artificial satellite is a system engineered to transmit different information from space to a ground control station. It is not a single system of communication but is a combination of complex multiple subsystems, which constantly communicate within the satellite with each other. This type of communication is intra-satellite communication. Currently, most of the satellites utilize a wired harness to provide power and signal connections for intra satellite communication, which results in a heavier system integration. This paper takes the approach towards wireless communication within the satellite using Bluetooth module HC-05 between the attitude and orbit control system(AOCS), sensors and actuators. The paper's objective is to reduce the weight of the satellites launched into orbit, in order to provide fewer thrust requirements. The system is based on Arduino Mega2560 and Lpc2148 which are being considered as two modules for the subsystems of a satellite.