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
* @description Orbital Object ToolKit (ootk) is a collection of tools for working
* with satellites and other orbital objects.
* @license AGPL-3.0-or-later
* @copyright (c) 2025 Kruczek Labs LLC
*
* Many of the classes are based off of the work of @david-rc-dayton and his
* Pious Squid library (https://github.com/david-rc-dayton/pious_squid) which
* is licensed under the MIT license.
*
* 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 { egm96Data, Egm96Entry } from './values/Egm96Data.js';
import { hpAtmosphereData } from './values/HpAtmosphereData.js';
import { HpAtmosphereResult } from './values/HpAtmosphereResult.js';
import { iau1980Data, Iau1980Entry } from './values/Iau1980Data.js';
import { leapSecondData } from './values/LeapSecondData.js';
/**
* Astrodynamic data management singleton.
*
* This class provides access to the various data sets used by the library.
* It is a singleton class, and can be accessed via the static
* [getInstance] method.
*/
export class DataHandler {
private static readonly instance_ = new DataHandler();
private constructor() {
// Prevent instantiation.
}
/**
* Returns the singleton instance of the DataHandler class.
* @returns The singleton instance of the DataHandler class.
*/
static getInstance(): DataHandler {
return DataHandler.instance_;
}
/**
* Retrieves the Egm96 coefficients for the given l and m values.
* @param l - The degree of the coefficient.
* @param m - The order of the coefficient.
* @returns The Egm96Entry object containing the coefficients.
*/
getEgm96Coeffs(l: number, m: number): Egm96Entry {
return egm96Data.getCoeffs(l, m);
}
/**
* Retrieves the IAU 1980 coefficients for the specified row.
* @param row The row index of the coefficients to retrieve.
* @returns The IAU 1980 entry containing the coefficients.
*/
getIau1980Coeffs(row: number): Iau1980Entry {
return iau1980Data.getCoeffs(row);
}
/**
* Retrieves the number of leap seconds for a given Julian date.
* @param jd The Julian date.
* @returns The number of leap seconds.
*/
getLeapSeconds(jd: number): number {
return leapSecondData.getLeapSeconds(jd);
}
/**
* Retrieves the atmosphere data for a given height.
* @param height The height for which to retrieve the atmosphere data.
* @returns The atmosphere data for the given height, or null if no data is available.
*/
getHpAtmosphere(height: number): HpAtmosphereResult | null {
return hpAtmosphereData.getAtmosphere(height);
}
}