ti_mo
45 lines
1.4 KiB
Matlab
45 lines
1.4 KiB
Matlab
satSim = create_satellite_sim(satConfig, groundStation);
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% viewer = satelliteScenarioViewer(satSim.sc);
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sampleTimes = satConfig.startTime:seconds(satConfig.sampleTime):satConfig.stopTime;
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distancesToSat = zeros(size(sampleTimes));
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elevationAnglesToSat = zeros(size(sampleTimes));
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progressStartText = "Starting ...";
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f = waitbar(0, progressStartText, "Name", "Task 1");
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progressTotal = numel(sampleTimes);
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progressQueue = parallel.pool.DataQueue;
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parfor_waitbar(f, progressTotal, progressStartText, true);
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progressListener = afterEach(progressQueue, @(info) parfor_waitbar(f, progressTotal, info, false));
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parfor idx = 1:numel(sampleTimes)
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res = perform_access_analysis(satSim, sampleTimes(idx));
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distancesToSat(idx) = res.distanceToSatellite;
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elevationAnglesToSat(idx) = res.elevationAngleToSatellite;
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send(progressQueue, sprintf("Index %d", idx));
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end
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delete(progressListener);
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if ishandle(f)
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close(f);
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end
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figure;
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plot(sampleTimes, distancesToSat);
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grid on;
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xlabel("Time [s]");
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ylabel("Distance to Satellite [m]");
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title("Distance over time plot of satellite pass");
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figure;
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plot(sampleTimes, elevationAnglesToSat);
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grid on;
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xlabel("Time [s]");
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ylabel("Elevation angle to satellite [degree]");
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title("Elevation angle over time plot of satellite pass");
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accessAnalysisResults.times = sampleTimes;
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accessAnalysisResults.distances = distancesToSat;
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accessAnalysisResults.elevationAngles = elevationAnglesToSat; |