Laplace Sphere Of Influence

Compute the Laplace sphere-of-influence scale a(m/M)^(2/5), not a Hill-stability radius.

Description

The Laplace sphere of influence is an approximate scale for changing a patched-conic reference body.

The Laplace sphere of influence is an approximate scale for changing a patched-conic reference body. It differs from the Hill radius and is not a sharp surface where only one body exerts gravity.1

Compute the Laplace sphere-of-influence scale a(m/M)^(2/5), not a Hill-stability radius.

When to use Laplace Sphere Of Influence

Use this tool to compute the Laplace sphere-of-influence scale a(m/M)^(2/5), not a Hill-stability radius.

Prepare the orbital state or model parameters in one reference frame. Confirm compatible distance/time units and the stated angular and gravitational-parameter conventions.

How to use Laplace Sphere Of Influence and understand its results

  1. Prepare the orbital state or model parameters in one reference frame. Confirm compatible distance/time units and the stated angular and gravitational-parameter conventions.
  2. Enter orbitalSemimajorAxis, secondaryMass, primaryMass using the field table and calculation rules, then run the tool.
  3. Read influenceRadius. The explanation below defines the units, signs, ordering and any flags or placeholder values.
  4. If the tool reports an input issue, correct the values and run it again. Apply the stated assumptions when interpreting a successfully returned result.
Input fieldMeaningValue type; see rules belowRequirement
orbitalSemimajorAxisOrbital semimajor axisnumberRequired
secondaryMassSecondary massnumberRequired
primaryMassPrimary massnumberRequired

Enter a positive orbital semimajor axis and positive common-unit masses, with secondary below primary. The tool applies the two-fifths mass-ratio power and returns a radius in the semimajor axis's unit.

influenceRadius = semimajorAxis × (secondaryMass/primaryMass)^0.4

Units, indexing, boundary conditions and exceptional cases are defined in the calculation rules above.

Output fieldMeaningValue type
influenceRadiusInfluence radiusnumber
json
{
  "input": {
    "orbitalSemimajorAxis": 10,
    "secondaryMass": 1,
    "primaryMass": 100000
  },
  "output": {
    "influenceRadius": 0.09999999999999998
  }
}

Limitations and assumptions

This is a small-secondary approximation without an ephemeris or force comparison. It does not select a hysteresis policy or establish Hill stability.

Numeric inputs must be finite. Follow the calculation-specific rules for overflow, underflow and exceptional cases. Missing required fields, extra fields, wrong value types and violations of the calculation rules are input errors.

Alternative or Complementary methods

Use Mutual Hill Separation: Compute mutual-Hill separation and screen a supplied boundary; the conventional 2√3 criterion assumes small, circular, coplanar two-planet orbits. For a complementary task, use Soi Handoff Hysteresis: Apply caller-defined sphere-of-influence handoff hysteresis to a sampled trajectory; boundaries are not universal force-dominance limits.

References

  1. Laplace Sphere Of Influence — tool.io

Similar or alternative tools

  • Mutual Hill Separation

    Compute mutual-Hill separation and screen a supplied boundary; the conventional 2√3 criterion assumes small, circular, coplanar two-planet orbits.

  • Soi Handoff Hysteresis

    Apply caller-defined sphere-of-influence handoff hysteresis to a sampled trajectory; boundaries are not universal force-dominance limits.

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