Simulation of Passive Magnetic Attitude Control System for Nano-Satellites. Uses SPG4 orbit propagator, IGRF Model for modelling earth's magnetic field.
Main Features Include:
- Computes all distubance torques.
- Calculates omega vector using Euler's Equations.
- Calculates power generation by solar panels, using sun vector determined by emperical formulae.
- Calculates State of charge of the battery as the satellite rotates in orbit.