C#调用STK输出卫星轨道数据的代码
时间: 2023-08-31 13:11:18 浏览: 336
STK实验卫星轨道参数仿真要点.doc
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以下是一个使用C#调用STK输出卫星轨道数据的示例代码:
```csharp
using System;
using AGI.STKObjects;
using AGI.STKUtil;
namespace STKExample
{
class Program
{
static void Main(string[] args)
{
// Create a new instance of STK
AgSTKObjectRoot stk = new AgSTKObjectRoot();
// Set the path to the STK scenario
string scenarioPath = "C:\\MySTKScenarios\\MyScenario.sc";
// Load the STK scenario
stk.LoadScenario(scenarioPath);
// Get the satellite object
AgSatellite satellite = (AgSatellite)stk.CurrentScenario.Children["Satellite1"];
// Get the orbit state data provider for the satellite
AgDataProvider orbitStateDataProvider = satellite.DataProviders["Orbit State"];
// Set the start and stop times for the data to be output
string startTime = "1 Jul 2021 00:00:00.000";
string stopTime = "10 Jul 2021 00:00:00.000";
// Set the time step for the data to be output (in seconds)
double timeStep = 60;
// Get the result of the data provider for the specified time range and time step
IAgDrResult result = orbitStateDataProvider.Exec(startTime, stopTime, timeStep);
// Get the array of orbital state data (position and velocity) from the result
double[,] orbitStateData = (double[,])result.DataSets.GetDataSetByName("Cartesian Position").GetValues();
// Output the orbital state data
for (int i = 0; i < orbitStateData.GetLength(0); i++)
{
Console.WriteLine("Time: " + result.DataSets.GetDataSetByName("Time").GetValues().GetValue(i));
Console.WriteLine("Position X: " + orbitStateData[i, 0]);
Console.WriteLine("Position Y: " + orbitStateData[i, 1]);
Console.WriteLine("Position Z: " + orbitStateData[i, 2]);
Console.WriteLine("Velocity X: " + orbitStateData[i, 3]);
Console.WriteLine("Velocity Y: " + orbitStateData[i, 4]);
Console.WriteLine("Velocity Z: " + orbitStateData[i, 5]);
Console.WriteLine();
}
// Release STK resources
stk.CloseScenario();
stk.Quit();
}
}
}
```
请注意,此代码仅为示例,需要根据实际情况进行修改。此外,您需要安装STK软件并具备一定的STK编程知识才能运行此代码。
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