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spacetime / Assure

Synthetic signal-loss demo

When signals disappear.

See how uncertainty grows as signals fail—and changes when they return. These are simulated values, not a live mission.

One Earth. Many ways to understand it.
Historical imagery · geographic context

Simulated comparison

What changes when a signal fails?

Compare uncertainty at a point 60 m ahead, inside a 40 m wide example corridor. Choose a condition below. Both views use the same model.

Uncertainty in the Numbers view is one standard deviation (σ).

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Held baseline · 0 s

Open sky

−20 m+20 m60 m0 m

±2.566 m

Pointwise 95% lateral interval · 60 m ahead

Inside the illustrative boundary

Margin 17.434 m · primary source · age 0 s

Selected condition · 75 s

Last-known fallback

−20 m+20 m60 m0 m

±35.308 m

Pointwise 95% lateral interval · 60 m ahead

Crosses the illustrative boundary

Margin -15.308 m · emergency source · age 35 s

At 75 s, the interval is ±35.308 m; the margin is -15.308 m. This is a computed illustration, not a measured position or an assurance decision.

What follows

Make the limits visible.

The authored interval widens through source loss and crosses the illustrative corridor in the fallback condition. Reacquiring evidence narrows it under this model. That result follows from the chosen assumptions; it does not prove that a real navigation system detects every failure.

A navigation interface should expose evidence age and applicability alongside its estimate. This experiment motivates that design question; it does not establish a validated policy.

Inspect the model, assumptions and limits

First-order propagation: σ² lateral(d) = σ² position + d²σ² heading. The interval is ±1.95996398454σ. Heading uses radians; position and distance use meters. Position and heading errors are assumed independent, zero-mean Gaussian variables.

  • No measured positioning accuracy, integrity protection level or trajectory guarantee.
  • The source-loss and recovery sequence and all sensor coefficients are authored.
  • The returned sigmaTerrain field is not used in the lateral-interval calculation.
  • Historical examples are context, not endorsement or direct technical lineage.

No empirical sensor or participant comparison is included; correlated errors, bias and incorrect assumptions can invalidate the illustrated coverage. Empirical comparison, participant testing and external peer review are not recorded for this investigation.

Inspect the exact model ↗

fog-fpv-1.2 · SHA-256 b1ecf9a53d781de1a26125077c13eeac5ae2cb4a374375e950eff84d8784ea69

Open the full Research experiment ↗
Navigation background

Knowledge carried between people.

The Polynesian Voyaging Society describes navigation using stars, the sun and ocean swells, and Nainoa Thompson’s learning from Satawal navigator Mau Piailug.

Read the primary account ↗

Time carried by an instrument.

Royal Museums Greenwich records Harrison’s H4 longitude watch, completed in 1759. It offers a historical example of turning a navigation question into a testable instrument.

Inspect the collection record ↗

For modern technical context, Cambridge’s An introduction to inertial navigation explains how errors accumulate and how additional information can constrain drift.

Data

Use the same evidence.

Download all 121 simulated states, or just the comparison shown above. Each includes the sources and limits.

Record, version and agent queryOpen the canonical public record ↗

For INT-001-SOURCE-LOSS, revision 2026-09-25-r1, compare elapsed 0 s and 75 s. What supports the finding, what assumptions could invalidate it, and what remains unknown? Include source IDs and limits.

curl -fsS https://noahlucas.com/spacetime-intelligence/v1/source-loss.json | jq '{id, revision, baseline: .samples[0], selected: .samples[75], limitations}'

Read-only public record. No agent writes, machine control, onboard deployment, or operational validity is granted by this export.

Record SHA-256 9c1804ea5e66e56a1d048e2cb8c644dfcc14d1ecd78ad75b169be348bc138f5c

The next question

Bring a capture to the question.

Open the capture viewer with your own supported recording, or try its synthetic example. Inspect timestamps, source and frame while keeping observations distinct from model assumptions.