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theory.","homepage":"https://github.com/behaver/elp2000-moon-gecc#readme","keywords":["moon","elp2000"],"repository":{"type":"git","url":"git+https://github.com/behaver/elp2000-moon-gecc.git"},"author":{"name":"Sanwan, Dong"},"bugs":{"url":"https://github.com/behaver/elp2000-moon-gecc/issues"},"license":"MIT","readme":"# ELP2000MoonGECC\n\n[![GitHub license](https://img.shields.io/badge/license-MIT-brightgreen.svg)](#) [![npm version](https://img.shields.io/npm/v/react.svg?style=flat)](https://www.npmjs.com/package/@behaver/elp2000-moon-gecc) [![PRs Welcome](https://img.shields.io/badge/PRs-welcome-brightgreen.svg)](#)\n\n## 简介\n\nELP2000MoonGECC 是计算月球的动力学 Date 地心平黄道坐标的组件库，其算法基于 ELP2000 理论。\n\n核心组件 ELP2000 计算器文档，另见：[ELP2000Calculator](./doc/ELP2000Calculator.md)\n\n## 安装\n\n通过 npm 安装，在你的 node 项目目录下执行：\n\n`npm install @behaver/elp2000-moon-gecc`\n\n安装完成后，调用即可：\n\n`const MoonGECC = require('@behaver/elp2000-moon-gecc');`\n\n## 用例\n\n```js\nconst MoonGECC = require('@behaver/elp2000-moon-gecc');\nconst { JDateRepository } = require('@behaver/jdate');\n\nlet jdr = new JDateRepository(2446896);\nlet moon = MoonGECC(jdr);\n\n// 获取月球地心黄经度数\nlet l = moon.l.getDegrees();\n\n// 获取月球地心黄纬度数\nlet b = moon.b.getDegrees();\n\n// 获取月球地心距离\nlet r = moon.r;\n\n// 获取月球地心球坐标\nlet sc = moon.sc;\n```\n\n关于计算误差的设置：\n\n```js\nconst MoonGECC = require('@behaver/elp2000-moon-gecc');\nconst { JDateRepository } = require('@behaver/jdate');\n\nlet jdr = new JDateRepository(2446896);\nlet moon = MoonGECC(jdr);\n\n// 方法一：调整精度等级\nmoon.accuracy = 'low';\n\n// 方法二：设置计算截断值数组\nmoon.setTruncation('b', [ 20, 10, 5, 3 ]);\n\n// 方法三：\n// 设置最大误差（瞬时）\nmoon.setMaxError('r', 5);\n\n// 设置平均最大误差\nmoon.setMaxError('r', 5, 'mean');\n\n// 设置安全最大误差\nmoon.setMaxError('r', 5, 'safe');\n```\n\n## API\n\n`constructor(jdate)`\n\n构造函数\n\n* jdate 参照儒略时间\n\n`get l()`\n\n获取 月球 Date 地心黄经值\n\n`get b()`\n\n获取 月球 Date 地心黄纬值\n\n`get r()`\n\n获取 月球 Date 地心距离，单位：km\n\n`get sc()`\n\n获取 月球 Date 地心黄道球坐标\n\n`get meanLongitude()`\n\n获取 月球 Date 地心平黄经\n\n`get longitudePerturbationCorrection()`\n\n获取 月球 Date 地心黄经摄动修正\n\n`get longitudePrecessionCorrection()`\n\n获取 月球 Date 地心黄经岁差修正\n\n`get obTime()`\n\n获取观测儒略时间\n\n`set obTime(jdr)`\n\n设定观测儒略时间\n\n* jdr 儒略时间对象\n\n`get accuracy()`\n\n获取计算精度\n\n`set accuracy(level)`\n\n设置计算精度\n\n* levev 包括以下几个等级：low, normal, high, fine, complete。\n\n精度等级和安全最大误差（单位：角秒, km）的对应关系：\n\n* low      5s, 10km \n* normal   2.5s, 5km\n* high     1s, 2km\n* fine     0.5s, 1km\n* complete 0\n\n此处不考虑 ELP2000 数据算法自身误差，实际误差要进行叠加。\n\n`getTruncation(item)`\n\n获取截断值数组\n\n* item 计算项：l、b、r\n\n`setTruncation(item, tNumsArray)`\n\n设置截断值数组\n\n* item 计算项：l、b、r\n* tNumsArray 截断值数组\n\n`setMaxError(item, value, mode = 'true')`\n\n设置计算允许最大误差\n\n通过此方法设置运算截断值相较于 `setTruncation(item, tNumsArray)` 和 `set accuracy(level)` 会产生额外的运算量，若为了缩小运算量而使用该方法，则不适于多次调用。\n\n* item 计算项：l、b、r\n* value 最大误差数值\n* mode 计算模式: true(瞬时误差)、mean(平均误差)、safe(安全误差)\n\n`getMaxError(item)`\n\n获取最大误差\n\n* item 计算项：l、b、r\n\n## 许可证书\n\nThe MIT license.\n","readmeFilename":"readme.md"}