Swarm Dynamics Simulator
Monte Carlo simulation for Dyson swarm station-keeping, collision probability, and propulsion authority analysis. Investigates the trade-offs between solar radiation pressure (SRP) control and active propulsion systems.
Swarm Parameters
Comparison Mode
Compares 7 spacing configurations (100m to 10,000m) while keeping other parameters constant. Identifies optimal spacing for collision probability vs control authority.
Configuration Summary
Collision Probability vs Spacing
Run a comparison simulation to see collision probability chart
Simulation Results
Configure the swarm parameters and run the simulation to see results.
Research Questions Addressed
RQ-1-2
Station-keeping propellant budget for maintaining orbital position
RQ-1-6
Collision probability between swarm elements at various spacings
RQ-1-37
Propulsion authority requirements for swarm control
Simulation Methodology
This Monte Carlo simulation models the station-keeping dynamics of a Dyson swarm segment, accounting for solar radiation pressure, orbital perturbations, and collision risk.
- Solar radiation pressure provides propellant-free thrust for attitude and position control
- Orbital perturbations include solar gravity gradient, third-body effects, and differential SRP
- Collision probability uses gas kinetics model with close approach event simulation
- Control authority compares available SRP delta-V to required station-keeping budget
Key trade-off: Closer spacing increases collision risk but reduces swarm volume; wider spacing improves safety but may exceed SRP control authority for maintaining formation.
This simulator also addresses RQ-1-2: Station-keeping propellant budget and RQ-1-37: Propulsion actuation authority