ZeqTrajectory — Multi-Body Optimization

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

Endpoint	POST /api/space/trajectory/optimize
Auth	api-key
Rate limit	10/min
Category	space

Parameters

Name	Type	Required	Description
origin	string	Yes	Departure body.
destination	string	Yes	Target body.
departureWindow	number	No	Search window in days. Default: 365.
payloadKg	number	No	Payload mass.

Returns

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

Example

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

This protocol is a named building block — one of the operations you compose inside a state contract. Call it directly with the request above, or invoke it from a contract that fires on your machine's clock. Browse the whole library at GET /api/protocols; fetch this one at GET /api/protocols/zeq-trajectory.