nauaneed / CompleteAttDetSim

Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink

Complete Simulation of Attitude Determination for a Satellite

Contents

1. Reference Vector Models

   1.1. Model of magnetic filed around earth(IGRF)

   1.2. Sun Vector Model

2. Sensor Models (Body Vector)

   2.1. Magnetometer Model

   2.2. Sun Sensor Model

3. Optimised TRIAD Attitude Determination Algorithm

4. J2 Orbit Propagator

5. Attitude Propagator

6. VRML object for visualisation