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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 { DifferentiableFunction } from '../main.js'; export declare class GoldenSection { private static readonly _grInv; private static check_; /** * Search for an optimal input value for function [f] that minimizes the * output value. * * Takes [lower] and [upper] input search bounds, and an optional * search [tolerance]. * @param f Function to optimize * @param lower Lower bound * @param upper Upper bound * @param root0 Root0 * @param root0.tolerance Root0.tolerance * @param root0.solveMax Root0.solveMax * @returns The optimal input value. */ static search(f: DifferentiableFunction, lower: number, upper: number, { tolerance, solveMax, }: { tolerance?: number; solveMax?: boolean; }): number; }