一、双行根数TLE下载
网上有一些下载最新双行根数的网站,例如:
- http://celestrak.com/ 无需注册可直接下载
- https://space-track.org/ 需要注册才能下载
二、利用STK Components做预报
- 新建控制台项目,并添加对
AGI.Foundation.Core.dll
和AGI.Foundation.Models.dll
的引用 - 完整代码如下
using System;
using AGI.Foundation;
using AGI.Foundation.Celestial;
using AGI.Foundation.Coordinates;
using AGI.Foundation.Geometry;
using AGI.Foundation.Propagators;
using AGI.Foundation.Time;
namespace Example005
{
class Program
{
static void Main(string[] args)
{
string license = "....需要有效的lic....";
Licensing.ActivateLicense(license);
// 定义需预报的时间区间
JulianDate start = new JulianDate(new DateTime(2020, 8, 13, 0, 0, 0));
JulianDate stop = new JulianDate(new DateTime(2020, 8, 13, 0, 10, 0));
// 定义1分钟间隔
var oneMinute = new Duration(0, 60);
// 给定卫星根数
string line1 = "1 25544U 98067A 20226.06311231 .00000634 00000-0 19556-4 0 9992";
string line2 = "2 25544 51.6462 66.9823 0001637 29.7739 108.2756 15.49160058240839";
// 创建卫星的运动点
var sgp4 = new Sgp4Propagator(new TwoLineElementSet(line1 + "\n" + line2));
PropagatorPoint satPoint = sgp4.CreatePoint();
// 直接预报TLE坐标系下的位置和速度
// Evaluate的order参数,0阶只求位置,1阶求位置和速度,2阶求位置、速度和加速度
DateMotionCollection<Cartesian> posList = satPoint.GetEvaluator().Evaluate(start, stop, oneMinute, 1);
WritePosList("TLE坐标系", posList);
// 获取地球
EarthCentralBody earth = CentralBodiesFacet.GetFromContext().Earth;
// 预报地固系下的位置和速度
PointEvaluator satPointInFixed = GeometryTransformer.ObservePoint(satPoint, earth.FixedFrame);
DateMotionCollection<Cartesian> posListInFixed = satPointInFixed.Evaluate(start, stop, oneMinute, 1);
WritePosList("地固坐标系", posListInFixed);
// 预报惯性坐标系下的位置和速度
PointEvaluator satPointInIcrf = GeometryTransformer.ObservePoint(satPoint, earth.InternationalCelestialReferenceFrame);
DateMotionCollection<Cartesian> posListInIcrf = satPointInIcrf.Evaluate(start, stop, oneMinute, 1);
WritePosList("惯性坐标系", posListInIcrf);
// 角度转弧度
double d2r = Math.PI / 180;
// 预报相对于测站的方位、仰角和距离
// 先定义测站位置
var stationPoint = new PointCartographic(earth, new Cartographic(120 * d2r, 30 * d2r, 100));
// 定义测站坐标轴和坐标系,xyz三轴为北东下右手坐标系
var stationAxes = new AxesNorthEastDown(earth, stationPoint);
var stationReferenceFrame = new ReferenceFrame(stationPoint, stationAxes);
// 在测站坐标系下观察卫星点
PointEvaluator satPointInStation = GeometryTransformer.ObservePoint(satPoint, stationReferenceFrame);
DateMotionCollection<Cartesian> posListInStation = satPointInStation.Evaluate(start, stop, oneMinute, 0);
// 卫星在测站坐标系下的位置值转换为方位、仰角和斜距
Console.WriteLine("测站坐标系");
for (int i = 0; i < posListInStation.Count; i++)
{
JulianDate time = posListInStation.Dates[i];
Cartesian pos = posListInStation.Values[i];
var aer = new AzimuthElevationRange(pos);
Console.WriteLine("{0:yyyy-MM-dd HH:mm:ss} {1,9:0.0000} {2,9:0.0000} {3,14:0.000}",
time.ToDateTime(), aer.Azimuth / d2r, aer.Elevation / d2r, aer.Range / 1000);
}
Console.ReadKey();
}
/// <summary>
/// 屏幕输出时间、位置和速度
/// </summary>
/// <param name="posList"></param>
static void WritePosList(string header, DateMotionCollection<Cartesian> posList)
{
Console.WriteLine(header);
for (int i = 0; i < posList.Count; i++)
{
JulianDate time = posList.Dates[i];
Cartesian pos = posList.Values[i]; // Values中存储的是位置
Cartesian vel = posList.FirstDerivatives[i]; // FirstDerivatives中存储的是速度
Console.WriteLine("{0:yyyy-MM-dd HH:mm:ss} {1,9:0.000} {2,9:0.000} {3,9:0.000} {4,9:0.000} {5,9:0.000} {6,9:0.000}",
time.ToDateTime(), pos.X / 1000, pos.Y / 1000, pos.Z / 1000, vel.X / 1000, vel.Y / 1000, vel.Z / 1000);
}
Console.WriteLine();
}
}
}
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