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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 { J2000, Kilometers } from '../main.js'; import { ObservationOptical } from './../observation/ObservationOptical.js'; type SolveOptions = { nRev?: number; direction?: boolean; posSearch?: number; velSearch?: number; tolerance?: number; printIter?: boolean; }; /** * Gooding angles-only initial orbit determination. * * Used for orbit determination from multiple optical observations. */ export declare class ModifiedGoodingIOD { private readonly observations_; private readonly mu_; constructor(observations: ObservationOptical[], mu?: number); private createInitial_; private _createErrorFunction; solve(r0: Kilometers, rN: Kilometers, { nRev, direction, posSearch, velSearch, tolerance, printIter, }: SolveOptions): J2000; } export {};