ADCS

STUDSAT

Attitude Determination & Control System

Objective
The attitude of a spacecraft is its orientation in space. The determination of attitude and controlling it to the requirement within the tolerance is a part of attitude determination and control. It projects the feasibility study and describes the preliminary analysis of both the position of the satellite centre of mass in three dimensional space and the methods to determine and control the orientation of the satellite with respect to its centre of mass in three dimensional spaces thus stabilising the satellite in the orbit. Thus works accordingly to point the camera of the satellite towards Nadir within tolerance.

Specification
STUDSAT

Coils specification
STUDSAT