Interactive workbench
Interactive demos for orbit propagation and collision avoidance. This is the interface skeleton; the compute service is wired in a later release.
- Orbital period
- —min
- J2 drift (RAAN)
- —deg/day
- Current subpoint
- —
- Numerical model
- —
- Last request
- —ms
| Times | Position Xkm | Position Ykm | Position Zkm | Altitudekm | Latitudedeg | Longitudedeg |
|---|
Preset scenes
Slot for picking one of 12 presets (later release)
Sample scenes are generated by the scene generator.
Live generation
Avoidance controls
- Optimal direction (ECI)
- —
- ΔV for a 1 km miss
- —m s⁻¹
- Current collision probability
- —
- NN policy (solid blue)
- No manoeuvre (dashed grey)
- SOCP expert (orange)
Generate or pick a scene in Scene setup first
Neural policy inference 0%
- Minimum miss distance
- —m
- Peak collision probability
- —
- Cumulative delta-v
- —m s⁻¹ expert —
- ΔV ratio (NN ÷ SOCP)
- —
Cumulative delta-v comparison
Three entry points
Each entry lands on a different position of the workbench
Orbit propagation and ground track
Tune altitude, eccentricity, inclination and RAAN; inspect the two-body plus J2 orbit shape and its ground track.
Enter the demo →Conjunction scene generation
Open a preset instantly, or generate single, multi-debris and adversarial cascaded conjunction geometries from a seed.
Enter the demo →Avoidance solving: impulse and low thrust
Compare the analytic single-impulse optimum with low-thrust policies on miss distance, collision probability and cumulative velocity increment.
Enter the demo →About this demo
- Hardware
- Intel Celeron J1900 @ 1.99 GHz · 4 cores · no GPU (pure CPU inference) · 7.6 GB RAM
- Software
- —
- Model file
- —
- Data
- Every computation runs on this machine; no data is uploaded.
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