Cubesat ADCS code written by Zarvan Movdawalla and Team, from MPSTME Mumbai.

A gymnaisum environment for autonomous decision making in fixed-wing aircraft

Aerospace Simulation and Training Resource Application

Physics-informed propellant combustion and nozzle performance simulator with an optional TensorFlow surrogate for specific impulse. Computes exhaust velocity, thrust, Isp, temp/pressure profiles, wall heating, and stability spectrum for multiple propellants. CLI, plots, and cached models in models