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ootk

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Orbital Object Toolkit including Multiple Propagators, Initial Orbit Determination, and Maneuver Calculations.

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/** * @author @thkruz Theodore Kruczek * @license AGPL-3.0-or-later * @copyright (c) 2025 Kruczek Labs LLC * * Orbital Object ToolKit is free software: you can redistribute it and/or modify it under the * terms of the GNU Affero General Public License as published by the Free Software * Foundation, either version 3 of the License, or (at your option) any later version. * * Orbital Object ToolKit is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; * without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. * See the GNU Affero General Public License for more details. * * You should have received a copy of the GNU Affero General Public License along with * Orbital Object ToolKit. If not, see <http://www.gnu.org/licenses/>. */ import { EpochUTC, EpochWindow, Seconds } from '../main.js'; // / Interpolator base class. export abstract class Interpolator { // Return the start and end epoch covered by this interpolator. abstract window(): EpochWindow; /* * Return `true` if the provided [epoch] is within this interpolator's * cached value range. */ inWindow(epoch: EpochUTC): boolean { const start = this.window().start; const stop = this.window().end; return start <= epoch && epoch <= stop; } /* * Calculate the start/stop epoch between this and another [Interpolator]. * * Returns `null` if there is no overlap between interpolators. */ overlap(interpolator: Interpolator): EpochWindow | null { const x1 = this.window().start; const x2 = this.window().end; const y1 = interpolator.window().start; const y2 = interpolator.window().end; if (x1 <= y2 && y1 <= x2) { const e1 = new EpochUTC(Math.max(x1.posix, y1.posix) as Seconds); const e2 = new EpochUTC(Math.min(x2.posix, y2.posix) as Seconds); return new EpochWindow(e1, e2); } return null; } }