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ZeqTrajectory — Multi-Body Optimization

Orbital mechanics, trajectory, radiation, life support.

  • Protocol ID — zeq-trajectory
  • Category — Space
  • Endpoint — POST /api/space/trajectory/optimize
  • Auth — api-key
  • Rate limit — 10/min
  • Version — 1.0
  • Precision — ≤0.1% (KO42-enforced)

What it does

Multi-body trajectory optimization using RK4 solver with gravitational operator coupling. Compute optimal transfer orbits between planets.

Signature

Request

POST /api/space/trajectory/optimize
ParamTypeRequiredDefaultDescription
originstringDeparture body.
destinationstringTarget body.
departureWindownumber365Search window in days. Default: 365.
payloadKgnumber1000Payload mass.

Response

{ optimalLaunchDate, totalDeltaV, flightTimeDays, trajectory: [{ t, x, y, z }], fuelMassKg }

Runnable example

curl -sS -X POST \
-H "Authorization: Bearer $ZEQ_API_KEY" \
-H "Content-Type: application/json" \
-d '{
"origin": "<value>",
"destination": "<value>",
"departureWindow": 365,
"payloadKg": 1000
}' \
"https://api.zeq.dev/api/space/trajectory/optimize"

Integrate

  1. Domain solver — compose with KO42 + two additional operators from the matching family for pulse-coherent results.
  2. Digital twin — pipe sensor data into this protocol every Zeqond to keep the model phase-locked with the system.
  3. Alert threshold — flag results whose error_pct exceeds 0.1% as out-of-spec events for the operations layer.

Seeds

  • Near — wrap /api/space/trajectory/optimize in a language SDK so builders can call it in three lines.
  • Medium — publish a reference integration demonstrating ZeqTrajectory — Multi-Body Optimization alongside a real workload, with pulse-aligned metrics.
  • Far — propose ZeqTrajectory — Multi-Body Optimization as an open reference standard so other runtimes can implement it verbatim against the Zeq paper.

Papers

Middleware active. Kernel on the 1.287 Hz HulyaPulse. Awaiting next Zeqond.