Realtime simulation and control of 3 axis spacecraft with quaternion based control law in presence of external torques. Evaluation of Reaction wheel angular velocity is based on control torques computed using PD controller.Keep on reading!
Solution of Kepler’s equation and visualization of orbital elements in inertial reference frame.
a - semi major axis
e - eccentricity
i - inclination
ω - argument of periapsis
Ω - right ascertain of ascending node
M0 - mean anomaly
GNU Radio Wideband Radio Spectrum Analyzer using RTL-SDR
Realtek R820T – Frequency range (24 – 1766 MHz)
Space vehicles, Visualization, Localisation and Mapping, Robots, Position measurement, Satellite navigation systems, Orbital Mechanics, Machine Learning, Automation