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Aegis BMD

CODENAME: AEGIS
GRPOReinforcement LearningC++JavaScriptNeural Network

Overview

Aegis BMD is Elston Industries' flagship ballistic missile defense simulation platform. It models a complete intercept engagement chain — from initial radar detection through threat discrimination, intercept solution computation, and kinetic engagement — using a fully autonomous AI agent trained via reinforcement learning.

The system is designed as both a research platform for exploring RL-based autonomous weapons control and a demonstration of low-latency, high-confidence engagement decision-making.


Reinforcement Learning Engine

Algorithm: GRPO

The interceptor control agent is trained using Group Relative Policy Optimization (GRPO), a variant of PPO that normalizes advantages across a sampled group of trajectories rather than using a value function baseline.

ParameterValue
Policy ArchitectureMulti-layer Perceptron (MLP)
Hidden Layers3 × 256 units
ActivationReLU
Group Size16 trajectories
Clip Epsilon0.2
Entropy Coefficient0.01

Reward Structure

The reward function is shaped to incentivize:

Training Environment

The simulation runs at 60Hz physics with stochastic threat injection. Threats vary in:


Threat Discrimination

The platform includes a multi-hypothesis tracker that maintains a probability distribution over threat class (ballistic, maneuvering, decoy) using a Kalman filter bank with interacting multiple model (IMM) estimation.

track_update(obs):
  for each model m in {ballistic, maneuver, decoy}:
    predict(m)
    update_likelihood(m, obs)
  mix_probabilities()
  return fused_state_estimate

Discrimination confidence gates engagement authority — the interceptor will not commit until P(threat) > 0.92.


Intercept Geometry

The engagement planner solves a proportional navigation intercept problem in 3D space using a predicted intercept point (PIP) algorithm:

  1. Estimate threat state via tracker
  2. Propagate threat trajectory forward using current model
  3. Solve intercept geometry for interceptor launch angle and time-of-flight
  4. Validate flyout kinematics against interceptor energy budget
  5. Commit launch

The guidance law transitions from proportional navigation to augmented PN in the terminal phase to compensate for late-breaking threat maneuvers.


Performance

All figures are simulation-derived and represent median performance across 10,000 Monte Carlo engagements in the standard threat library.


Stack