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SCIENCE · INVESTIGATE AND EXPLAIN

Test orbital invariants against an independent exact trajectory

A numerical orbit can preserve one invariant while accumulating trajectory error. Use the normalized central field μ = 1 and initial position (1, 0), velocity (0, 1). The exact orbit is the unit circle with period 2π, energy per mass −0.5 and angular momentum per mass 1.

Learning outcome: Compare Euler and Verlet on two grids, saving invariant extrema and endpoint position/velocity errors with the exact reference.

Starting recap

Integrate mass moments about named axes, derive torque and angular-momentum constraints, and test orbital energy, angular and numerical consistency against independent evidence.

All lessons are open directly. Your saved experiments remain when you leave and return.

Try

The exact endpoint after one period is position (1, 0) and velocity (0, 1). Any nonzero discrepancy in this stipulated noiseless benchmark is numerical, not an observation error. Halving the step changes the approximation, not the target reference.

Open the experiment

Predict

If Verlet preserves angular momentum to rounding in this benchmark, that alone establishes:

Experiment

Compare Euler and Verlet on two grids, saving invariant extrema and endpoint position/velocity errors with the exact reference.

Compare orbital invariants with trajectory error

Worked teaching model · synthetic values · Normalized mu=1, initial r=(1,0),v=(0,1),exact circular period2pi. Compare forward Euler and velocity Verlet over that fixed interval. Point source and bounded numerical benchmark, not real orbital prediction.

Reset keeps your prediction, captures and practice history.

One exact-period numerical benchmark

north position (m)east position (m)-1.01193611.006149-1.004949

Spatial axes use the same pixels per physical unit, preserving geometry. 1: computed trajectory (solid).2: exact circular reference (dashed). Joined curves show the supplied model, not additional observations.

Equivalent numerical coordinates for One exact-period numerical benchmark

computed trajectory

east position (m)north position (m)
10
0.9876630.1570796
0.95096190.3102844
0.89081810.4558401
0.80873860.5901711
0.70677470.7099916
0.5874660.8123884
0.45377220.8948925
0.30899430.9555374
0.15668870.9929038
0.00057666811.006149
-0.15554940.9950206
-0.30791810.9598573
-0.45286950.9015723
-0.58694060.821627
-0.70694450.7219896
-0.81004160.6050857
-0.8938020.4737377
-0.9562580.3310977
-0.99594570.1805744
-1.0119360.02575452
-1.003855-0.129678
-0.9718885-0.2820251
-0.9167838-0.4276577
-0.8398291-0.5630979
-0.7428295-0.6850982
-0.628068-0.7907169
-0.4982564-0.8773882
-0.3564768-0.9429846
-0.2061121-0.9858711
-0.05076987-1.004949
0.1058019-0.999689
0.259804-0.9701485
0.4074783-0.916979
0.5452015-0.8414159
0.6695771-0.7452533
0.7775238-0.6308048
0.8663563-0.5008491
0.9338579-0.3585618
0.9783401-0.207436
0.9986893-0.05119336

At most 82 representative computed coordinates including endpoints; the plotted curve can use a finer grid. A table of a revealed generator is not independent measurement evidence.

exact circular reference

east position (m)north position (m)
10
0.99691730.0784591
0.98768830.1564345
0.97236990.2334454
0.95105650.309017
0.92387950.3826834
0.89100650.4539905
0.85264020.5224986
0.8090170.5877853
0.7604060.649448
0.70710680.7071068
0.6494480.760406
0.58778530.809017
0.52249860.8526402
0.45399050.8910065
0.38268340.9238795
0.3090170.9510565
0.23344540.9723699
0.15643450.9876883
0.07845910.9969173
6.12323e-171
-0.07845910.9969173
-0.15643450.9876883
-0.23344540.9723699
-0.3090170.9510565
-0.38268340.9238795
-0.45399050.8910065
-0.52249860.8526402
-0.58778530.809017
-0.6494480.760406
-0.70710680.7071068
-0.7604060.649448
-0.8090170.5877853
-0.85264020.5224986
-0.89100650.4539905
-0.92387950.3826834
-0.95105650.309017
-0.97236990.2334454
-0.98768830.1564345
-0.99691730.0784591
-11.22465e-16
-0.9969173-0.0784591
-0.9876883-0.1564345
-0.9723699-0.2334454
-0.9510565-0.309017
-0.9238795-0.3826834
-0.8910065-0.4539905
-0.8526402-0.5224986
-0.809017-0.5877853
-0.760406-0.649448
-0.7071068-0.7071068
-0.649448-0.760406
-0.5877853-0.809017
-0.5224986-0.8526402
-0.4539905-0.8910065
-0.3826834-0.9238795
-0.309017-0.9510565
-0.2334454-0.9723699
-0.1564345-0.9876883
-0.0784591-0.9969173
-1.83697e-16-1
0.0784591-0.9969173
0.1564345-0.9876883
0.2334454-0.9723699
0.309017-0.9510565
0.3826834-0.9238795
0.4539905-0.8910065
0.5224986-0.8526402
0.5877853-0.809017
0.649448-0.760406
0.7071068-0.7071068
0.760406-0.649448
0.809017-0.5877853
0.8526402-0.5224986
0.8910065-0.4539905
0.9238795-0.3826834
0.9510565-0.309017
0.9723699-0.2334454
0.9876883-0.1564345
0.9969173-0.0784591
1-2.44929e-16

At most 82 representative computed coordinates including endpoints; the plotted curve can use a finer grid. A table of a revealed generator is not independent measurement evidence.

Calculated quantities under the declared measurement model
QuantityValueUnit
Step size0.1570796s
Maximum sampled specific energy error7.33904e-5m²/s²
Maximum sampled specific angular momentum error3.33067e-16m²/s
Endpoint position error0.05121013m
Endpoint velocity error0.05112682m/s
Final specific energy-0.5m²/s²

Conserved angular momentum or small energy drift does not alone establish the correct orbital phase.

The exact reference returns to its initial state at2pi. Forward Euler uses old velocity and acceleration; velocity Verlet uses a position drift with half acceleration and averages old/new accelerations for velocity. The central-force Verlet steps preserve angular momentum up to rounding, but finite-step trajectory error remains. Compare two grids and both invariants with the independent exact endpoint.

Predict before inspecting the values. Save contrasting records with assumptions and one alternative explanation. This virtual display does not certify practical measurement technique.

Conserved angular momentum or small energy drift does not alone establish the correct orbital phase.

The exact reference returns to its initial state at2pi. Forward Euler uses old velocity and acceleration; velocity Verlet uses a position drift with half acceleration and averages old/new accelerations for velocity. The central-force Verlet steps preserve angular momentum up to rounding, but finite-step trajectory error remains. Compare two grids and both invariants with the independent exact endpoint.

Captures preserve recipes and replay their calculated results. They are synthetic model evidence, not physical measurements.

Understand

Test orbital invariants against an independent exact trajectory

A numerical orbit can preserve one invariant while accumulating trajectory error. Use the normalized central field μ = 1 and initial position (1, 0), velocity (0, 1). The exact orbit is the unit circle with period 2π, energy per mass −0.5 and angular momentum per mass 1.

Forward Euler advances position using old velocity and velocity using old acceleration. Velocity Verlet first advances position with the old acceleration correction, then updates velocity using the average of old and new accelerations. The two methods use the same force law but have different numerical structure.

For each supported step count, retain maximum sampled energy error and maximum sampled angular-momentum error, then compare endpoint position and velocity with the exact return at time 2π. A small endpoint energy discrepancy alone can conceal phase error or larger earlier errors. The exact reference is independent of either numerical trajectory.

For a central force, the Verlet drift/kick structure preserves angular momentum up to rounding, yet finite-step position error remains. Forward Euler generally drifts outward in this benchmark. Compare two step counts rather than treating one successful-looking plot as a guarantee for arbitrary eccentric or singular trajectories. The equal-scale graphic displays geometry honestly; no real satellite or mission prediction is implied.

Changed-case check

Predict before reading the comparison. The exact endpoint after one period is position (1, 0) and velocity (0, 1). Any nonzero discrepancy in this stipulated noiseless benchmark is numerical, not an observation error. Halving the step changes the approximation, not the target reference.

Retained investigation

Compare Euler and Verlet on two grids, saving invariant extrema and endpoint position/velocity errors with the exact reference. How can a method preserve angular momentum yet return to the wrong point after one exact period?

Source and boundary

Primary conceptual reference checked 30 October 2026: OpenStax University Physics Volume 1. All models, packets and teaching prose are original. These are bounded mathematical investigations, not measured apparatus, physical procedures, practical certification or institutional credit.

The specific numerical updates are documented in Andrew Cumming, PHYS 512: Symplectic integrators, checked 30 October 2026. Our finite-grid evidence task uses an independently specified exact circular reference.

Apply

If Verlet preserves angular momentum to rounding in this benchmark, that alone establishes:

Public practice checks a specific claim. It does not establish independent mastery.

How can a method preserve angular momentum yet return to the wrong point after one exact period?

Continue

Completion requires a saved prediction, at least one capture and a reflection. Presence checks do not grade your reasoning.

Skipping retains experiments and awards no mastery.

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