ootk
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Orbital Object Toolkit including Multiple Propagators, Initial Orbit Determination, and Maneuver Calculations.
44 lines (43 loc) • 1.95 kB
TypeScript
/**
* @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, J2000 } from '../main.js';
import { CubicSplineInterpolator } from './CubicSplineInterpolator.js';
import { LagrangeInterpolator } from './LagrangeInterpolator.js';
import { StateInterpolator } from './StateInterpolator.js';
/**
* Two-body Velocity Verlet Blend interpolator.
*
* The [VerletBlendInterpolator] retains the original ephemerides, so the
* original _"truth"_ states can be retrieved if needed without imparting any
* additional error, so this can be used to build other interpolator types.
* The implementation is simple and very tolerant when working with sparse
* ephemerides.
*/
export declare class VerletBlendInterpolator extends StateInterpolator {
ephemeris: J2000[];
constructor(ephemeris: J2000[]);
get sizeBytes(): number;
window(): EpochWindow;
private static getClosest_;
private matchState_;
private static _gravity;
private static integrate_;
interpolate(epoch: EpochUTC): J2000 | null;
getCachedState(epoch: EpochUTC): J2000 | null;
toCubicSpline(): CubicSplineInterpolator;
toLagrange(order?: number): LagrangeInterpolator;
}