Independent R&D Demo · Synthetic Data · Agency-Neutral

Synthetic Sensor / Digital-Twin T&E Lab

A repeatable test and evaluation environment for stressing sensing and tracking behavior before expensive physical trials. Apply the same synthetic truth and detections to two tracker configurations, map the operating envelope, sweep parameters, and rerun deterministic Monte Carlo tests by seed.

Digital-Twin TestbedSynthetic Sensors Same-Input ComparisonMonte Carlo Evaluation Operating EnvelopeVVUQ-Oriented T&E
73.6%

lower position RMSE on 120 held-out synthetic stress trials

Seventy-two candidate configurations were evaluated only on the calibration set. The selected configuration was frozen before the held-out stress evaluation.

97.4%held-out track continuity vs. 82.9% baseline
91.4%faster mean track confirmation
100%objects confirmed at least once vs. 95.2% baseline
240calibration + held-out deterministic stress trials
How to read the lab

Same synthetic world. Same observations. Two configurations.

The central visualization now compares the untuned baseline and T&E-selected tracker side by side. Both panels receive exactly the same truth trajectories, measurement noise, dropouts, latency, and clutter. Under easy conditions they look similar. Under mixed stress, the performance gap becomes visually obvious.

1 · EnvironmentGenerate truthRepeatable moving-object trajectories from a fixed seed.
2 · Sensor modelInject uncertaintyNoise, latency, dropout, detection probability, and clutter.
3 · System under testRun both configurationsExact same detections feed baseline and selected tracker.
4 · InstrumentationMeasure behaviorRMSE, continuity, confirmation, and stress sensitivity.
● Live same-input comparisonNominalTEST RUN DT-10482
Synthetic truth Sensor detection Clutter Baseline estimate T&E-selected estimate Delayed observation
Verified held-out synthetic benchmark

Configuration selection happens before the held-out stress set is scored.

The revised benchmark uses an actual 72-configuration sweep across 120 deterministic calibration trials. A robustness score selects one configuration. That configuration is then frozen and evaluated, together with the fixed baseline, on a separate 120-trial stress set.

73.6%

lower held-out RMSE

Mean position error for confirmed tracks across unseen stress trials.

20.77   →   5.49
97.4%

held-out continuity

Fraction of object-frame opportunities covered by a confirmed estimate.

82.9%   →   97.4%
91.4%

faster confirmation

Reduction in mean time needed to establish a confirmed track.

25.55 steps   →   2.20 steps
100%

objects ever confirmed

Fraction of held-out synthetic objects reaching confirmed-track state at least once.

95.2%   →   100%
Parameter-sweep heatmap

Calibration RMSE by smoothing gain and association gate

β = 0.05 and confirmation count = 2 are held fixed here for readability. Lower is better. The glowing cell is the selected region.

α ↓ / Gate →
12
18
24
0.40
35.43RMSE
17.90RMSE
8.31RMSE
0.55
33.41RMSE
17.18RMSE
7.22 ★selected
0.70
34.71RMSE
18.32RMSE
7.53RMSE
0.85
36.43RMSE
19.84RMSE
9.43RMSE
Synthetic operating envelope

Selected configuration under combined noise + dropout

Each cell shows RMSE / continuity from 100 deterministic trials with Pd=90%, latency=2, and clutter=2/frame.

σ ↓ / Drop →
5%
10%
20%
30%
2
2.498.0%
2.597.8%
2.697.0%
2.796.0%
4
4.298.0%
4.297.8%
4.397.0%
4.596.0%
6
6.197.9%
6.297.7%
8.597.0%
7.795.8%
8
15.397.3%
12.197.3%
17.596.0%
18.094.6%
Browser quick-check

Run 100 lightweight deterministic stress trials

Ready. This quick-check is separate from the verified 120-trial held-out benchmark above.
—trials where selected RMSE beats baseline
—mean baseline RMSE
—mean selected RMSE
—selected mean continuity
Held-out benchmark detail

Same 120 unseen stress trials, two frozen configurations.

MetricUntuned baselineT&E-selected
Position RMSE20.775.49
Track continuity82.9%97.4%
Mean confirmation latency25.552.20
Objects ever confirmed95.2%100%
Selected configuration

Frozen before held-out evaluation

  • α = 0.55 measurement-position correction.
  • β = 0.05 velocity correction.
  • Association gate = 24 synthetic position units.
  • Confirmation count = 2 consistent observations.
  • Maximum unobserved persistence = 6 frames before track deletion.
  • The baseline uses a simple position smoother, gate 15, confirmation count 3, and two-frame persistence.
72candidate configurations
120calibration trials
120held-out trials
10objects per benchmark trial
80frames per trial
5stress dimensions varied
High-level T&E architecture

Model. Stress. Compare. Measure. Validate.

01 · Model

Digital-twin scenario

Define truth trajectories, object populations, scenario geometry, and sensor-observation abstractions.

02 · Stress

Uncertainty injection

Control detection probability, measurement noise, latency, dropout, clutter, and scenario density.

03 · Compare

Same-input systems

Feed identical observations to baseline and candidate configurations so differences are attributable to the system under test.

04 · Measure

Performance instrumentation

Calculate continuity, position error, confirmation latency, track persistence, and stress sensitivity.

05 · Validate

Hold-out evaluation

Freeze selected settings and test them on disjoint stress cases before reporting generalization.

Research questions

A credible digital-twin lab should reveal boundaries, not just averages.

1

Where does the system break?

Map continuity and error as sensing becomes noisier, delayed, less available, or more cluttered.

2

Which parameters matter?

Use controlled sweeps to identify sensitivity to association gates, confirmation requirements, and filter gains.

3

Does tuning generalize?

Evaluate selected settings on disjoint held-out stress trials instead of reporting the tuning set.

4

What is the operating envelope?

Quantify the range of uncertainty over which continuity and error remain acceptable.

5

What should move to physical testing?

Use simulation to identify boundary cases that justify scarce hardware, facility, or field-test resources.

6

Can every run be reproduced?

Preserve test IDs, seeds, configurations, stress settings, and evaluation partitions.

Multi-domain relevance

The methodology is reusable across sensing, autonomy, and monitoring problems.

Autonomous Perception

Stress tracking and perception behavior before moving selected boundary cases into physical tests.

Multi-Sensor Fusion

Explore how uncertainty, latency, clutter, and missing observations affect fused estimates and confidence.

Maritime & Undersea Systems

Evaluate generic sensing and tracking behavior under sparse, delayed, noisy, or intermittent observations.

Industrial Digital Twins

Test virtual sensing, monitoring, and control assumptions before changing physical systems or production workflows.

Transportation & Logistics

Stress asset tracking against missing reports, location noise, delay, and false observations.

Infrastructure Monitoring

Evaluate sensor-network resilience and detection behavior across controlled failure and uncertainty conditions.

Research leadership

Systems evaluation, simulation, data engineering, and AI/ML in one integrated team.

SD

Dr. Sajib Datta

Principal Investigator · Systems, Data & T&E Lead

Technical direction, digital-twin architecture, data pipelines, experiment design, uncertainty injection, reproducibility, performance measurement, integration, and evaluation methodology.

TD

Dr. Tonmoay Deb

Co-Investigator · AI/ML & Modeling Lead

Predictive modeling, sensor/data fusion, confidence-aware AI, synthetic scenario design, robustness analysis, parameter optimization, and AI/ML evaluation.

Public technical context

Grounded in digital-twin validation, uncertainty quantification, and virtual testing.

NIST · Digital Twins for Advanced Manufacturing

NIST emphasizes reliable, interoperable, trustworthy digital twins and explicitly identifies Verification, Validation, and Uncertainty Quantification for data, models, and digital-twin results.

Public reference ↗
NIST · Digital Twins Workshops Summary Report

The 2026 report identifies VVUQ, interoperability, cybersecurity, and trustworthy scalable digital twins as ongoing research and standards priorities.

Public reference ↗
NASA JSTAR · Software Digital Twins

NASA describes software digital twins that emulate hardware, simulate sensors and actuators, integrate operational software, and expand test resources before physical-system availability.

Public reference ↗
Independent, nonproprietary research disclaimer.
This page is an independent Omniscient Innovations LLC research demonstration using deterministic synthetic, non-sensitive data. It is agency-neutral and is not sponsored, funded, endorsed, certified, selected, or validated by any government entity or other organization. The browser laboratory and benchmark intentionally use simplified public-facing sensor and tracker abstractions to demonstrate test-and-evaluation methodology without disclosing proprietary algorithms, operational interfaces, controlled technical information, CUI, classified information, export-controlled data, or Government-furnished information. The synthetic models are not physics-accurate replicas of any specific operational sensor. All performance values on this page are synthetic experimental results from the described benchmark and must not be interpreted as fielded, operational, mission-certified, or independently validated performance.