Astrophyzix Technical Transparency Report · Computational Methods & NASA Integration
Float64 · IEEE‑754 · Yoshida‑4 · Runge–Kutta · Dormand–Prince · N‑Body · WebGPU · VSOP87 · NASA APIs
✨ A detailed public outreach explainer in response to user questions about how Astrophyzix computes, refines, and visualises orbits of planets, potentially hazardous asteroids (PHA'S), comets and Near-Earth Objects (NEO's)
High‑Order Integrators NASA API Integration
Introduction
Astrophyzix is committed to transparent science communication. This report explains — in clear, technical detail — the numerical standards, integrators, GPU compute systems, and NASA data pipelines that power the Astrophyzix Digital Observatory.
Numerical Foundations — Float64 & IEEE‑754
Astrophyzix performs all orbital calculations using Float64, the 64‑bit floating‑point format defined by the IEEE‑754 standard. This provides:
- ~15–17 digits of precision
- stable rounding behaviour
- predictable error propagation
- compatibility with NASA Horizons and JPL SBDB data
Lower‑precision formats (Float32) introduce rounding errors that accumulate into kilometre‑scale deviations over long integrations. Float64 ensures:
- accurate MOID calculations
- stable long‑term orbit propagation
- precise close‑approach modelling
- correct gravitational‑keyhole geometry
High‑Order Integrators — RK4, Dormand–Prince & Yoshida‑4
Runge–Kutta 4 (RK4)
RK4 is a fourth‑order integrator ideal for short‑term propagation and real‑time visualisation. Astrophyzix uses RK4 for:
- interactive orbital viewers
- short‑arc propagation
- educational simulations
Dormand–Prince (RKF45)
Dormand–Prince is an adaptive Runge–Kutta method that adjusts timestep size based on error. Astrophyzix uses it for:
- long‑term orbital evolution
- uncertainty modelling
- Monte‑Carlo refinement
Yoshida‑4 (Symplectic Integration)
Yoshida‑4 is a symplectic integrator that preserves:
- total system energy
- angular momentum
- orbital shape
Astrophyzix uses Yoshida‑4 for:
- long‑term N‑Body simulations
- gravitational‑keyhole analysis
- planetary‑defence modelling
N‑Body Physics — Real Gravitational Dynamics
Astrophyzix uses full N‑Body gravitational modelling to simulate:
- planetary perturbations
- lunar influence
- solar tides
- resonances
- long‑term orbital drift
This is essential because real asteroids do not follow perfect ellipses — their paths are shaped by every major gravitational body in the Solar System.
VSOP87 — High‑Precision Planetary Ephemerides
VSOP87 provides milliarcsecond‑level planetary positions. Astrophyzix uses VSOP87 to:
- initialise planetary positions
- drive N‑Body simulations
- align with NASA Horizons
Accurate asteroid modelling requires accurate planetary positions — VSOP87 ensures this.
WebGPU — GPU‑Accelerated Scientific Computing
WebGPU allows Astrophyzix to run:
- parallel N‑Body simulations
- GPU‑accelerated integrators
- real‑time orbital visualisation
This makes Astrophyzix one of the only public observatories running scientific‑grade physics entirely client‑side, without downloading, without logging in, without intrusive ads and without compromising or hiding any of the data. This isn't marketing, it's fully verified by our provenance and governance documentation which is included with every tool.
NASA API Integration — What Each API Provides
| NASA API | What It Provides | How Astrophyzix Uses It |
|---|---|---|
| JPL SBDB | Orbital elements, uncertainties, physical parameters, MOID, condition codes | Initialises orbital solutions, updates refinement engine |
| CNEOS CAD | Close‑approach tables, nominal/min/max distances, velocities | Generates close‑approach reports & risk assessments |
| NASA Scout | Impact probabilities, short‑arc solutions, uncertainty regions | Cross‑checks early‑stage NEOs & validates refinement outputs |
| NASA Horizons | High‑precision ephemerides, state vectors, barycentric positions | Feeds N‑Body engines & long‑term propagation |
| NASA NeoWs | Discovery data, basic orbital info, public‑facing updates | Provides metadata & discovery context |
How Astrophyzix Performs Orbital Refinement
Astrophyzix treats every asteroid as a live, evolving dataset. When new observations appear in MPC, SBDB, or Scout, the system
- Fetches updated orbital elements & uncertainties via NASA APIs
- RK4 (short‑term)
- Dormand–Prince (adaptive)
- Yoshida‑4 (long‑term symplectic)
- Runs N‑Body perturbation modelling
- Computes refined MOID, close‑approach geometry, and uncertainty regions
- Updates the Astrophyzix Orbital Viewer in real time
How Astrophyzix Generates SBDB‑Style Orbital Visualisations
Astrophyzix’s orbital viewer is designed to match the clarity and scientific accuracy of the NASA SBDB Orbital Viewer. It uses:
- WebGPU for rendering orbital paths
- Float64 state vectors for precision
- VSOP87 planetary positions for accuracy
- N‑Body perturbations for realism
- adaptive integrators for smooth propagation
The result is a visualisation that:
- matches NASA Horizons ephemerides
- reflects real gravitational dynamics
- updates instantly when new NASA data arrives
Scientific Summary
• IEEE‑754 Float64 precision
• High‑order integrators (RK4, RKF45, Yoshida‑4)
• GPU‑accelerated N‑Body physics via WebGPU
• VSOP87 planetary ephemerides
• Live NASA data streams (SBDB, CNEOS, Scout, Horizons, NeoWs)
This fusion of authoritative data and high‑precision computation allows Astrophyzix to operate as a public‑facing digital observatory capable of real‑time orbital refinement, accurate close‑approach modelling, and transparent planetary‑defence analysis. Each module we build is offered as an open access public tool. We copyright register our modules to protect the integrity of our platform and the information we provide.