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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, Vector, Vector3D } from '../main.js'; import { Thrust } from './Thrust.js'; export declare class ForceModel { private _centralGravity?; private _thirdBodyGravity?; private _solarRadiationPressure?; private _atmosphericDrag?; private _maneuverThrust; setGravity(mu?: number): this; setEarthGravity(degree: number, order: number): void; setThirdBodyGravity({ moon, sun }: { moon?: boolean | undefined; sun?: boolean | undefined; }): void; setSolarRadiationPressure(mass: number, area: number, coeff?: number): void; /** * Sets the atmospheric drag for the force model. * @deprecated This is still a work in progress! * @param mass - The mass of the object. * @param area - The cross-sectional area of the object. * @param coeff - The drag coefficient. Default value is 2.2. * @param cosine - The cosine of the angle between the object's velocity vector and the drag force vector. */ setAtmosphericDrag(mass: number, area: number, coeff?: number, cosine?: number): void; loadManeuver(maneuver: Thrust): void; clearManeuver(): void; acceleration(state: J2000): Vector3D; derivative(state: J2000): Vector; }