anyground
04 / Universal modularity

Precision Service Dock

Three spherical contacts, six contact constraints and separate service islands make a common interface tangible. Modularity begins at the connection—not at the shape of the building.

3D ENGINEERING EXPLORER / Loading assemblyProposed hardware · dimensioned explanatory model
ANYGROUND / INTERFACEAssembly overview

Loading local 3D geometry. The complete technical dossier remains below.

Drag to orbit · scroll / pinch to zoom · click a part to inspect. Keyboard: focus model, arrows to orbit, + / − to zoom. Flow dots indicate routing, not simulated flow rates.

Operating sequence /

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Inputs
Outputs
Failure boundary

HOW TO BUILD IT

Let rough structures meet precise machines.

A mechanism, a materials choice, a resource boundary and a falsifiable experiment—not a claim of completed hardware.

The precision service dock

The unexpected connection: a telescope fixture becomes a habitat interface

Universal modularity breaks down when it is asked to do too many jobs in one connection. A rough building joint, a fluid seal, a machine reference and a robot docking target have different requirements. The useful combination is not a more elaborate universal plug. It is a small precise datum carried by a forgiving structural system, with resources connected separately.

Precision-machine kinematic couplings provide the starting principle. Three spherical contacts engage three differently oriented V-grooves, creating six nominal point contacts. A separate preload keeps the contacts seated. This avoids the geometrical ambiguity of forcing two imperfect broad surfaces against each other. The design principle is established; the adaptation to dirty crop/service cassettes is an Anyground proposal. MIT coupling guidance

The same datum convention could serve a root-zone cassette, a camera calibration fixture, a pump carrier or a seed-metering cartridge. That does not make their payloads, utilities, sanitation or hazards interchangeable. Each variant declares its own mass, center of gravity, materials, resources and acceptance tests.

Walk through the mechanism

1. The structure carries load; the local datum carries a reference

The lower plate bolts to the stable service edge. It does not ask a foldable canopy or a long aluminum rail to maintain precision at every point. Local calibration can reference the plate after deployment. If a frame flexes or moves, the system checks the relationship between the robot and the station rather than assuming a factory calibration still holds.

A proposed 620 × 520 mm plate in this demonstrator is an authored bench size, not an optimized product. Actual thickness, supports and allowable loading follow a stiffness study. A flexible plate carrying beautiful precision contacts is still a poor fixture.

2. Three balls meet six contact rails

The visible upper carrier holds three spheres. Beneath each is a pair of parallel radial round rails that form a V-like groove. Their orientations differ around the plate. Each sphere contacts two rails; the six contact normals nominally constrain the six rigid-body degrees of freedom.

The model uses a 25 mm sphere radius, a 12 mm rail radius and 18 mm half-separation. The sphere's center must sit above the rail centers by:

h = sqrt((R + r)² − d²)

For these proposed dimensions, h ≈ 32.33 mm. The depicted contacts therefore meet by construction, rather than by an illustrator placing a ball approximately above a groove. This is a geometric check. It does not calculate contact deformation, friction, stiffness, load capacity or final repeatability.

3. Preload is independent of location

A locating contact is not a latch. The separate clamp arrangement closes the contacts and resists the allowed disturbance. Excess force deforms the contact; too little permits lift-off. Forces from hoses, robot acceleration and an eccentric payload matter.

The displayed clamps are static explanatory hardware. The cycle does not claim to demonstrate an autonomous clamp actuator. A bench experiment can begin with manual clamps while it establishes the datum's usefulness. Automating a coupling before measuring its re-seating error would confuse two development questions.

4. Utility islands remain separate

The right-hand bracket illustrates distinct resource positions. The coupling's balls are not electrical contacts, and the grooves are not sealing surfaces. A mechanically repeatable location can guide a separately compliant utility connector toward its mating part, but the connector must have its own rated geometry, engagement allowance and verification.

A nutrient branch, potable branch and dirty return cannot be distinguished only by software. Use physically incompatible connector families, durable markings and resource-specific qualification. A common mounting footprint is a catalog convenience, not permission to mix media.

5. The dry-break cutaway exposes the residual-fluid problem

The simplified cutaway shows a spring, seal and closing element. It explains how a disconnected service can limit release, but it is not a vendor's proven internal design. Actual materials, pressure, flow resistance, food-contact suitability, contamination, cleanability and seal life are unresolved until a connector is selected and tested.

The intended service sequence is stop, isolate, prove safe, contain residuals, disconnect, exchange, reconnect, test and recommission. Do not treat a successful robot motion command as evidence of a safe fluid connection.

6. Identity and physical evidence agree before enable

The label links a part to a revision and resource record. The depicted pattern is not an actual scannable production code. A physical engagement sensor offers a different kind of information. Neither is sufficient alone: a valid label can be on the wrong part, and a stuck switch can report a seat that is not secure.

Each process adds its own return-to-service measurement, such as leak and actual flow, or an electrical protection check. The local protective controller retains authority; an AI planner may diagnose or propose work without overriding these boundaries. NASA hardware guidance informs this design discipline, not certification of this fixture. NASA hardware guidance

How it changes the whole platform

The precision interface connects two scales that are usually kept apart. A habitat kit can tolerate practical regional manufacturing and field adjustment, while a small process station carries a measured, replaceable reference. A robot does not need to discover every soft leaf, panel edge and pipe by unconstrained perception if the task is designed around known carriers and calibration datums.

This suggests a progression: first locate a carrier manually; then prove one robotic approach; then qualify one safe service exchange; finally replicate the station. The common advantage is accumulated fixture and recovery knowledge, not a slogan about plug-and-play everything.

Exact-constraint fixtures are not a new invention. The research question is whether this architecture measurably reduces handling and servicing work in the proposed combined living/production system. The first experiment should measure that reduction against an ordinary bolted drawer and commercial tool changer.

Build the first bench

Use the proposed geometry and BOM as a test article, not a manufacturing drawing. The downloadable scene coordinates explain arrangement, but omit production tolerances, contact finishes and safety calculations. Start with a harmless dummy payload and manual clamps. Add a robot only after the datum and extraction route are useful.

The planning allowance is USD 400–1,500 for a small bench's material/component scope. It is an authored allowance, not a supplier quote; outsourced machining, a robot, engineering labor, qualification and water testing can dominate the real cost.

Run fifty removal/re-seating cycles with a fixed documented preload and payload. Measure several axes, report the distribution and repeat after deliberately introducing known debris. A proposed screening target is a 95th-percentile position error below 0.10 mm; this is a test threshold, not an achieved specification. Try wrong revisions and ambiguous engagement. The process must remain disabled rather than make a confident-looking guess.

Only then add a separately qualified low-risk wet loop. Measure release, leak rate and pressure drop; freeze connector-specific limits before testing. If dust, hose forces or payload bending consume the positioning allowance, redesign the protection and local reference before claiming robotic interchangeability.

PROTOTYPE BOOK

Parts. Procedure. Pass / fail.

Authored engineering allowances—not supplier quotations. No hardware purchased. Open the detailed records for scope, dimensions, test methods and cost exclusions.

Open the complete prototype specification
id
interface-bench-01
status
Proposed experiment — not performed
objective
Determine whether one exact-constraint datum can make repeated robotic/manual carrier replacement practical without coupling fluid sealing to precision location.
proposed Dimensions
base M
  • 0.62
  • 0.05
  • 0.52
ball Radius M
0.025
groove Rod Radius M
0.012
rail Half Separation M
0.018
bom
  • item
    Machined reference and carrier plates
    quantity
    2
    material
    Aluminum alloy selected for stiffness/corrosion requirements
  • item
    Replaceable spherical contacts
    quantity
    3
    material
    Hardened steel, surface quality to be specified
  • item
    Radial groove contact rails
    quantity
    6
    material
    Hardened round steel inserts
  • item
    Adjustable retention clamps
    quantity
    3
    material
    Rated industrial clamps, not precision locators
  • item
    Media-specific connector pair
    quantity
    1
    material
    Select after fluid/pressure/sanitation review; not a universal plug
  • item
    Seat sensor and independent displacement measurement
    quantity
    2
    material
    Local switch plus dial indicator or calibrated displacement sensor
planning Cost
currency
USD
range
  • 400
  • 1500
basis
Authored bench planning allowance, not supplier quotes
excludes
  • machining labor if outsourced
  • robot
  • certification
  • safety review
  • water-quality testing
  • engineering labor
tests
  • test
    Clean re-seating
    method
    Fifty manual remove/reseat cycles at a fixed declared preload; measure position in multiple axes and record distribution, not only the best result
    target
    Proposed screening target: 95th percentile error below 0.10 mm under the declared payload. Not a demonstrated rating.
  • test
    Debris and wrong-part rejection
    method
    Introduce known dust/debris and an incorrect module revision; detect or reject ambiguous states
    target
    No process enable when identity or physical engagement is uncertain
  • test
    Retention and stiffness
    method
    Apply a controlled representative disturbance load, with protective enclosure and engineering review
    target
    No unintended separation; report force/deflection and permanent offsets
  • test
    Isolated wet exchange
    method
    Use a separately qualified low-risk water test loop and measure actual residual release, pressure drop and leaks after exchange
    target
    Freeze connector-specific limits before test; datum accuracy alone is not acceptance
stop Condition
Change the contact protection or station reference if dust, payload deformation or service connection forces consume the allowable robot positioning error.
PRIMARY EVIDENCE

Follow the evidence.

Access levels distinguish full papers, abstracts, institutional reports and technical documentation. Findings belong to the cited devices; our proposed integration must earn its own results.

I01 / REFERENCE · full text

Kinematic couplings for rapid and repeatable positioning ↗

Finding. Three spheres against three V-grooves provide six nominal contacts; exact-constraint design separates location from other functions.

Design use. Explicit contact geometry, independent preload and a repeatability experiment.

Boundary. The performance of existing precision fixtures is not the performance of this proposed dusty field interface.

I02 / REFERENCE · official documentation

Hardware and Equipment — NASA human integration guidance ↗

Finding. Hardware interfaces should prevent incorrect installation and support correct handling and verification.

Design use. Separate media keying, physical engagement, identity and return-to-service evidence.

Boundary. Guidance does not qualify an Anyground coupling, hazard-control system or connector.