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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/>. */ export declare class PolynomicalRegressionResult { coefficients: Float64Array; rss: number; bic: number; /** * Create a new [PolynomicalRegressionResult] object, containing the * polynomial [coefficients], root-sum-squared error [rss], and Bayes * information criterea [bic]. * @param coefficients The polynomial coefficients. * @param rss The root-sum-squared error. * @param bic The Bayes information criterea. * @returns The optimal input value. */ constructor(coefficients: Float64Array, rss: number, bic: number); }