finalized plotting utility
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@@ -19,6 +19,7 @@ classdef miSim
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barrierExponent = NaN; % CBF exponent parameter
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minAlt = 0; % minimum allowable altitude (m)
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artifactName = "";
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f; % main plotting tiled layout figure
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fPerf; % performance plot figure
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end
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@@ -31,7 +32,6 @@ classdef miSim
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% Plot objects
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makePlots = true; % enable/disable simulation plotting (performance implications)
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makeVideo = true; % enable/disable VideoWriter (performance implications)
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f; % main plotting tiled layout figure
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connectionsPlot; % objects for lines connecting agents in spatial plots
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graphPlot; % objects for abstract network graph plot
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partitionPlot; % objects for partition plot
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@@ -1,9 +1,11 @@
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function f = plotGpsLogs(logDirs)
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function [f, G] = plotGpsLogs(logDirs, seaToGroundLevel)
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arguments (Input)
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logDirs (1, 1) string;
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seaToGroundLevel (1, 1) double = 110; % measured approximately from USGS national map viewer for the AERPAW test field
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end
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arguments (Output)
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f (1, 1) matlab.ui.Figure;
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G cell;
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end
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% Plot setup
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f = uifigure;
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@@ -17,9 +19,6 @@ function f = plotGpsLogs(logDirs)
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% configured data
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params = readScenarioCsv(scenarioCsv);
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% coordinate system constants
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seaToGroundLevel = 110; % meters, measured approximately from USGS national map viewer
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fID = fopen(fullfile(matlab.project.rootProject().RootFolder, "aerpaw", "config", "client1.yaml"), 'r');
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yaml = fscanf(fID, '%s');
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fclose(fID);
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@@ -45,12 +44,19 @@ function f = plotGpsLogs(logDirs)
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% Automatically detect start/stop of algorithm flight (ignore takeoff, setup, return to liftoff, landing segments of flight)
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pctThreshold = 60; % pctThreshold may need adjusting depending on your flight
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startIdx = find(verticalSpeed <= prctile(verticalSpeed, pctThreshold), 1, 'first');
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stopIdx = find(verticalSpeed <= prctile(verticalSpeed, pctThreshold), 1, 'last');
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startIdx = find(verticalSpeed <= prctile(verticalSpeed, pctThreshold), 1, "first");
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stopIdx = find(verticalSpeed <= prctile(verticalSpeed, pctThreshold), 1, "last");
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% % Plot whole flight, including setup/cleanup
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% startIdx = 1;
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% stopIdx = length(verticalSpeed);
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% Convert LLA trajectory data to ENU for external analysis
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% NaN out entries outside the algorithm flight range so they don't plot
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enu = NaN(height(G{ii}), 3);
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enu(startIdx:stopIdx, :) = lla2enu([G{ii}.Latitude(startIdx:stopIdx), G{ii}.Longitude(startIdx:stopIdx), G{ii}.Altitude(startIdx:stopIdx)], lla0, "flat");
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enu = array2table(enu, 'VariableNames', ["East", "North", "Up"]);
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G{ii} = [G{ii}, enu];
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% Plot recorded trajectory over specified range of indices
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geoplot3(gf, G{ii}.Latitude(startIdx:stopIdx), G{ii}.Longitude(startIdx:stopIdx), G{ii}.Altitude(startIdx:stopIdx) + seaToGroundLevel, c(mod(ii, length(c))), 'LineWidth', 2, "MarkerSize", 5);
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@@ -58,7 +64,7 @@ function f = plotGpsLogs(logDirs)
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% Plot domain
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altOffset = 1; % to avoid clipping into the ground when displayed
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domain = [lla0; enu2lla(params.domainMax, lla0, 'flat')];
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domain = [lla0; enu2lla(params.domainMax, lla0, "flat")];
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geoplot3(gf, [domain(1, 1), domain(2, 1), domain(2, 1), domain(1, 1), domain(1, 1)], [domain(1, 2), domain(1, 2), domain(2, 2), domain(2, 2), domain(1, 2)], repmat(domain(1, 3) + altOffset, 1, 5), 'LineWidth', 3, 'Color', 'k');
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geoplot3(gf, [domain(1, 1), domain(2, 1), domain(2, 1), domain(1, 1), domain(1, 1)], [domain(1, 2), domain(1, 2), domain(2, 2), domain(2, 2), domain(1, 2)], repmat(domain(2, 3) + altOffset, 1, 5), 'LineWidth', 3, 'Color', 'k');
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geoplot3(gf, [domain(1, 1), domain(1, 1)], [domain(1, 2), domain(1, 2)], domain(:, 3) + altOffset, 'LineWidth', 3, 'Color', 'k');
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@@ -72,12 +78,12 @@ function f = plotGpsLogs(logDirs)
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% Plot objective
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objectivePos = [params.objectivePos, 0];
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llaObj = enu2lla(objectivePos, lla0, 'flat');
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llaObj = enu2lla(objectivePos, lla0, "flat");
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geoplot3(gf, [llaObj(1), llaObj(1)], [llaObj(2), llaObj(2)], [llaObj(3), domain(2, 3)], 'LineWidth', 3, "Color", 'y');
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% Plot obstacles
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for ii = 1:params.numObstacles
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obstacle = enu2lla([params.obstacleMin((1 + (ii - 1) * 3):(ii * 3)); params.obstacleMax((1 + (ii - 1) * 3):(ii * 3))], lla0, 'flat');
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obstacle = enu2lla([params.obstacleMin((1 + (ii - 1) * 3):(ii * 3)); params.obstacleMax((1 + (ii - 1) * 3):(ii * 3))], lla0, "flat");
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geoplot3(gf, [obstacle(1, 1), obstacle(2, 1), obstacle(2, 1), obstacle(1, 1), obstacle(1, 1)], [obstacle(1, 2), obstacle(1, 2), obstacle(2, 2), obstacle(2, 2), obstacle(1, 2)], repmat(obstacle(1, 3) + altOffset, 1, 5), 'LineWidth', 3, 'Color', 'r');
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geoplot3(gf, [obstacle(1, 1), obstacle(2, 1), obstacle(2, 1), obstacle(1, 1), obstacle(1, 1)], [obstacle(1, 2), obstacle(1, 2), obstacle(2, 2), obstacle(2, 2), obstacle(1, 2)], repmat(obstacle(2, 3) + altOffset, 1, 5), 'LineWidth', 3, 'Color', 'r');
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geoplot3(gf, [obstacle(1, 1), obstacle(1, 1)], [obstacle(1, 2), obstacle(1, 2)], obstacle(:, 3) + altOffset, 'LineWidth', 3, 'Color', 'r');
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@@ -1,10 +1,10 @@
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function f = plotRadioLogs(resultsPath)
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function [f, R] = plotRadioLogs(resultsPath)
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arguments (Input)
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resultsPath (1, 1) string;
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end
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arguments (Output)
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f (1, 1) matlab.ui.Figure;
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R cell;
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end
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logDirs = dir(resultsPath);
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@@ -1,14 +0,0 @@
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%% Plot AERPAW logs (trajectory, radio)
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resultsPath = fullfile(matlab.project.rootProject().RootFolder, "sandbox", "t1"); % Define path to results copied from AERPAW platform
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% Plot GPS logged data and scenario information (domain, objective, obstacles)
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fGlobe = plotGpsLogs(resultsPath);
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% Plot radio statistics
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fRadio = plotRadioLogs(resultsPath);
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%% Run simulation
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% Run miSim using same AERPAW scenario definition CSV
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%% Plot AERPAW trajectory logs onto simulated result for comparison
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66
aerpaw/results/resultsAnalysis.m
Normal file
66
aerpaw/results/resultsAnalysis.m
Normal file
@@ -0,0 +1,66 @@
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%% Plot AERPAW logs (trajectory, radio)
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resultsPath = fullfile(matlab.project.rootProject().RootFolder, "sandbox", "t1"); % Define path to results copied from AERPAW platform
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% Plot GPS logged data and scenario information (domain, objective, obstacles)
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seaToGroundLevel = 110; % measured approximately from USGS national map viewer
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[fGlobe, G] = plotGpsLogs(resultsPath, seaToGroundLevel);
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% Plot radio statistics
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[fRadio, R] = plotRadioLogs(resultsPath);
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%% Run simulation
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% Run miSim using same AERPAW scenario definition CSV
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csvPath = fullfile(matlab.project.rootProject().RootFolder, "aerpaw", "config", "scenario.csv");
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params = readScenarioCsv(csvPath);
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% Visualization settings
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plotCommsGeometry = false;
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makePlots = true;
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makeVideo = true;
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% Define scenario according to CSV specification
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domain = rectangularPrism;
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domain = domain.initialize([params.domainMin; params.domainMax], REGION_TYPE.DOMAIN, "Domain");
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domain.objective = domain.objective.initialize(objectiveFunctionWrapper(params.objectivePos, reshape(params.objectiveVar, [2 2])), domain, params.discretizationStep, params.protectedRange, params.sensorPerformanceMinimum);
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agents = cell(size(params.initialPositions, 2) / 3, 1);
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for ii = 1:size(agents, 1)
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agents{ii} = agent;
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sensorModel = sigmoidSensor;
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sensorModel = sensorModel.initialize(params.alphaDist(ii), params.betaDist(ii), params.alphaTilt(ii), params.betaTilt(ii));
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collisionGeometry = spherical;
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collisionGeometry = collisionGeometry.initialize(params.initialPositions((((ii - 1) * 3) + 1):(ii * 3)), params.collisionRadius(ii), REGION_TYPE.COLLISION, sprintf("Agent %d collision geometry", ii));
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agents{ii} = agents{ii}.initialize(params.initialPositions((((ii - 1) * 3) + 1):(ii * 3)), collisionGeometry, sensorModel, params.comRange(ii), params.maxIter, params.initialStepSize, sprintf("Agent %d", ii), plotCommsGeometry);
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end
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% Create obstacles
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obstacles = cell(params.numObstacles, 1);
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for ii = 1:size(obstacles, 1)
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obstacles{ii} = rectangularPrism;
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obstacles{ii} = obstacles{ii}.initialize([params.obstacleMin((((ii - 1) * 3) + 1):(ii * 3)); params.obstacleMax((((ii - 1) * 3) + 1):(ii * 3))], "OBSTACLE", sprintf("Obstacle %d", ii));
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end
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% Set up simulation
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sim = miSim;
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sim = sim.initialize(domain, agents, params.barrierGain, params.barrierExponent, params.minAlt, params.timestep, params.maxIter, obstacles, makePlots, makeVideo);
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% Save simulation parameters to output file
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sim.writeInits();
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% Run
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sim = sim.run();
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%% Plot AERPAW trajectory logs onto simulated result for comparison
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% Duplicate plot to overlay with logged trajectories
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comparison = figure;
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copyobj(sim.f.Children, comparison);
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% Plot trajectories on top
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hold(comparison.Children.Children(end), "on");
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for ii = 1:size(G, 1)
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plot3(comparison.Children(1).Children(end), G{ii}.East, G{ii}.North, G{ii}.Up + seaToGroundLevel, 'Color', 'r', 'LineWidth', 1);
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end
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hold(comparison.Children.Children(end), "off");
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@@ -1,2 +0,0 @@
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<?xml version="1.0" encoding="UTF-8"?>
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<Info location="plotResults.m" type="File"/>
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@@ -0,0 +1,2 @@
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<?xml version="1.0" encoding="UTF-8"?>
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<Info location="resultsAnalysis.m" type="File"/>
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