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KosmOSS

Python CI Rust CI

Lightning fast aerospace software.

Overview

KosmOSS is a comprehensive spacecraft simulation and control software stack written in Rust, with Python visualization tools. It includes:

  • Low-fidelity orbital mechanics simulation with Earth gravity model
  • Quaternion-based attitude dynamics and control
  • Hohmann transfer guidance for orbit raising/lowering
  • Real-time Earth orientation parameters (EOP) for coordinate transformations (pulled from Celestrak)
  • Low-fidelity atmospheric drag model
  • Interactive 3D mission visualization dashboard
  • Energy and angular momentum conservation tracking

KosmOSS is currently in an alpha state, providing a 6DOF simulation environment for spacecraft dynamics and control. Right now main.rs configures a simple ballistic trajectory for a spacecraft.

Requirements

Rust

  • Rust 2021 edition or later
  • Cargo package manager

Python (for visualization)

  • Python 3.10+
  • Required packages:
    • matplotlib
    • numpy
    • pandas
    • cartopy
    • pytest

Setup

  1. Clone the repository:
git clone https://github.com/Kosmos-Industries/KosmOSS.git
cd KosmOSS
  1. Install Python dependencies using Poetry:
poetry install

Usage

Running the simulation

cargo run --release

Visualizing the results

poetry run python viz/plotMissionDashboard.py

This will generate both static and interactive visualization dashboards showing:

  • 3D orbital trajectory
  • Spacecraft attitude
  • Control torques and thrust
  • Energy and angular momentum conservation
  • Ground track on Earth map

Finite State Machine (FSM)

The spacecraft simulation includes a state machine that manages different operational modes:

States

  • Safe Mode: Initial state with minimal system activity
  • Detumbling: Active attitude control to reduce angular velocity
  • Nominal Operation: Normal orbital operations
  • Maneuver Preparation: Pre-maneuver checks and preparation
  • Maneuvering: Active orbital maneuver execution
  • Emergency: Fault handling and recovery

State Transitions

  • Safe Mode → Detumbling: When angular velocity exceeds threshold
  • Detumbling → Nominal Operation: When angular velocity is stabilized
  • Nominal Operation → Maneuver Prep: When maneuver is commanded
  • Maneuver Prep → Maneuvering: After preparation period
  • Any State → Emergency: When angular velocity exceeds safety threshold
  • Emergency → Safe Mode: After recovery period

Control Authority

The FSM determines:

  • When attitude control can be applied
  • When orbital maneuvers can be executed
  • Safety constraints for spacecraft operations

Usage

The FSM automatically evaluates state transitions based on spacecraft dynamics and mission time. Maneuvers can only be commanded during Nominal Operation state.

Example state sequence: Safe Mode → Detumbling → Nominal Operation → Maneuver Prep → Maneuvering → Nominal Operation

Contributing

We welcome contributions! Please:

  1. Fork the repository
  2. Create a feature branch
  3. Make your changes
  4. Run tests and formatting:
cargo test
cargo fmt
poetry run pytest
poetry run ruff format
  1. Create a pull request

License

This project is licensed under the Apache 2.0 License. See the LICENSE file for details.