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;
}
}