✳ ASTROX/ 02
← MISSION ARCHIVE / AEROSPACE SIMULATOR

CIRRUS · SILENCE 8048

TECHNICAL PROJECT / ASTRA - Aerospace Simulator

A high-fidelity aerospace simulation environment designed to visualize orbital mechanics, spacecraft dynamics, and mission operations in real time. The simulator serves as both an engineering tool and an educational platform for aerospace system development.

2026_10

Source code ↗

Challenge

Create an accurate yet interactive simulation capable of reproducing realistic spacecraft behavior while remaining flexible enough for integrating future GNC, ADCS, and mission-planning modules.

Approach

Implemented a modular simulation engine combining orbital mechanics, spacecraft dynamics, visualization, and numerical integration techniques. The architecture emphasizes extensibility, allowing new spacecraft subsystems and control algorithms to be integrated with minimal modifications.

Outcome

Delivered a scalable spacecraft simulator suitable for validating aerospace algorithms, demonstrating orbital maneuvers, and supporting future research in autonomous space systems.

Tools

PythonNumPyMatplotlib

Roadmap

  1. Astra Space Simulator

    A high-fidelity spacecraft simulation environment designed to visualize orbital mechanics, spacecraft dynamics, and mission operations in real time. The simulator serves as both an engineering tool and an educational platform for spacecraft system development.

    Completed

MISSION CONSOLE / BROWSER RUN

CIRRUS · SILENCE 8048

Browser model · assumptions shown

Propagate an Earth two-body orbit and inspect altitude, speed and period. The model runs locally in this browser; it does not execute unpublished source code.

INITIAL CONDITIONS / MODEL PARAMETERS

SCHEMATIC 3D / DRAG TO ROTATE

Illustrative geometry; not the original CAD model.

Adjust the conditions, then run the simulation.

Model assumptions and limits

RELATED / SHARED TECHNOLOGIES

LAST LIGHT

GNC Completed

LAST LIGHT ↗

TECHNICAL PROJECT / Robust 6-DOF Guidance, Navigation and Control for Autonomous Powered Descent Under Wind, Navigation Uncertainty and Partial Actuator Degradation

The objective is to recover a six-degree-of-freedom vehicle from an initially descending, laterally displaced and deliberately tilted state, reject atmospheric wind and sensor uncertainty, command thrust and two-axis t…

Run simulation ↗

Find your next destination.

TAB TO NAVIGATE · ENTER TO OPEN · ESC TO CLOSE