Design and Implementation of On-Board Computer Sub-System for Picosat

Abstract

Satellite tracking and control module in charge of maintenance is the subsystem. Monitoring and control of satellite locations affect the environment. Satellites are subjected to torque. This causes alignment and satellite angle instability while it is in space. The project involves the implementation of a satellite system and a test tool technology platform able to have it for lunch in the near future. It is also aimed towards them. Investigate the use of low-cost cube sats in the realm of remote sensing. In the original iteration of their design, the cube satellite utilized Picosat passive attitude control. However, a new version has been released to fulfil the accuracy standards of Picosat, the primary payload, which was supposed to be active attitude control. New posture determination and control the subsystem is in charge of successfully de-tumbling Picosat after booting and keeping it pointed in the right direction. As much as feasible, the desired alignment. This chapter describes the concept and execution of strong decision-making.