Reference · Journey mode: transfers, launch windows and flip-and-burn trips
keplerfunction
Kepler's equation M = E - e sin E, solved for the eccentric anomaly by Newton's method.
Import it
import { kepler } from "@johnmorrisdotca/uchusen-rockets/journey";
Definition
function kepler(meanAnomaly: number, e: number): number
Parameters
| Name | Type | Description |
|---|---|---|
meanAnomaly | number | The mean anomaly, radians. |
e | number | The eccentricity, 0 to below 1. |
Returns
number
The eccentric anomaly, radians, in the same turn as the mean anomaly.
Examples
import { kepler } from "@johnmorrisdotca/uchusen-rockets/journey";
console.log(kepler(1, 0.2).toFixed(4));1.1853What it prints (run when this page was built)