A field team faces an unresolved physical question: Why does satellite geometry turn 6 metres into 39? They must answer it before changing separation on the real device. Predict the direction first.
See the relationship before changing it
The figure reads from left to right. The blue card is separation. The middle card applies this page's relationship. The green card is variance sum. Walk the arrows once: set the input, apply the rule, then read the result with its unit.
The retained audit below checks several chapter fixtures. This added model holds every other chapter fixture fixed, so the numeric fixture does not switch without explanation.
Derive the baseline in four named moves
- 1
Name the input. The chapter baseline for separation is 10.
- 2
Name the relationship. 1.5²+2.5²+5.0²+0.5²+1.0²+0.3² = 34.8 m² UERE = √34.8 = 5.90 m ≈ 6 m 6x1.5 = 9.0 m; 6x4.0 = 24.0 m; 6x6.5 = 39.0 m
- 3
Substitute the chapter fixture. Set separation to 10. The page ledger gives variance sum as 34.840.
- 4
Read the result. Keep the stated output unit beside the value. Use it only inside the technical boundary on this page.
Predict, then change separation
Try Predict the direction of variance sum. Move one control, calculate, then check your prediction.
Observe Clustered directions cannot separate position changes well, so the same range noise stretches into a larger location region. Reset the control to 10 and compare variance sum.
Explain Only separation moves here. The other chapter fixtures remain fixed.
Check yourself
What should you do before trusting a moved-control result?
What does this small model leave out?
1. Separate error size from error direction
Independent random errors can point positive or negative, so they partly cancel. Their variances always add. Geometry is different: it describes how the satellite directions turn the remaining range error into a position error.
2. Name every algebra move
Square each errorThis removes sign and creates variance.
Add variancesΣσ².
Undo the squareUERE=√Σσ².
Apply geometryσposition=GDOP×UERE.
3. Reproduce the chapter table
UERE = √34.8 = 5.90 m ≈ 6 m
6×1.5 = 9.0 m; 6×4.0 = 24.0 m; 6×6.5 = 39.0 m
The ionosphere contributes 25/34.8 = 71.8% of variance. Linear addition gives 10.8 m, 1.83× the root-sum-square result.
4. Try the satellite separation
TryMove two toy satellite directions apart and watch their geometry multiplier.
ObserveAt 10°, toy DOP is 8.14; at 90°, it falls to 1.41.
ExplainClustered directions cannot separate position changes well, so the same range noise stretches into a larger location region.
The slider is a two-direction, flat-world picture of a real matrix problem.
- Receiver
- Real GPS solves 3-D position plus clock bias
- Errors
- Root-sum-square assumes independence
- Confidence
- One sigma is not a guaranteed maximum
Use receiver covariance, satellite health, multipath tests, and the product's confidence rule.
5. Match accuracy to consequence
Use a wide, uncertain zone when the error supports only a hint. Require corrections, better geometry, fusion, or a guarded fallback before position can trigger a costly or safety-sensitive action.
6. Record the accuracy evidence
Store the error-source assumptions, satellite set, GDOP, covariance or confidence, age, environment, enhancement service, outage behavior, and field truth used to validate the claim.
7. Check yourself
Why not add the six errors directly?
What does GDOP=6.5 do to 6 m?
Does the two-satellite slider model real GPS?
The six errors and GDOP examples are the chapter's values; the two-direction DOP is a deliberately bounded teaching model.
- 5.90 m
- Exact chapter RSS
- 6 m
- Chapter rounded UERE
- √2/sin(φ)
- 2-D geometry illustration
Correct, not complete: this ledger does not qualify a receiver, correction service, or location-triggered action.
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