ootk
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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 } from '../main.js';
import { StateCovariance } from './../covariance/StateCovariance.js';
// / Batch least squares orbit determination result.
export class BatchLeastSquaresResult {
/**
* Create a new [BatchLeastSquaresResult] object, containing the solved
* [state], [covariance], and root-mean-squared error [rms].
* @param state The solved state.
* @param covariance The solved covariance.
* @param rms The root-mean-squared error.
*/
constructor(public state: J2000, public covariance: StateCovariance, public rms: number) {
// Nothing to do here.
}
}