تلخیص
This paper describes the design of space
environment module that is used for validation of Attitude
Determination and Control Systems (ADCS) control
algorithms for LEO Satellites. This module is the major block
of a complete AOCS simulator, the other blocks of which are
the sensors, actuators and control algorithms. The space
environment module includes orbit propagator, GPS time, Sun
model, magnetic field model and spacecraft attitude
kinematics and dynamics. The performance of the module will
1 spacecraft. The Kompsat-1
results are generated in Satellite Tool Kit (STK) which will
serve as a reference for space environment results verification
Umar Mufti, Atiq-ur-Rehman. (2011) Design of Space Environment module for Validation o Attitude Control Algorithms for LEO Satellites, Journal of Space Technology , Volume 1, Issue 1.
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