first aerpaw test prepared

aerpaw/results/plotGpsLogs.m

@@ -1,7 +1,8 @@
-function [f, G] = plotGpsLogs(logDirs, seaToGroundLevel)
+function [f, G] = plotGpsLogs(logDirs, seaToGroundLevel, plotWholeFlight)
     arguments (Input)
         logDirs (1, 1) string;
         seaToGroundLevel (1, 1) double = 110; % measured approximately from USGS national map viewer for the AERPAW test field
+        plotWholeFlight (1, 1) logical = false;
     end
     arguments (Output)
         f (1, 1) matlab.ui.Figure;
@@ -48,8 +49,10 @@ function [f, G] = plotGpsLogs(logDirs, seaToGroundLevel)
         stopIdx = find(verticalSpeed <= prctile(verticalSpeed, pctThreshold), 1, "last");
     
         % % Plot whole flight, including setup/cleanup
-        % startIdx = 1;
-        % stopIdx = length(verticalSpeed);
+        if plotWholeFlight
+            startIdx = 1;
+            stopIdx = length(verticalSpeed);
+        end
 
         % Convert LLA trajectory data to ENU for external analysis
         % NaN out entries outside the algorithm flight range so they don't plot

aerpaw/results/readRadioLogs.m

@@ -31,14 +31,26 @@ function R = readRadioLogs(logPath)
         end
 
         fid = fopen(filepath, 'r');
-        % Skip 3 lines: 2 junk (tail errors) + 1 header (tx_uav_id,value)
-        for k = 1:3
-            fgetl(fid);
+        % Skip header lines: some files have 2 tail-error lines + 1 column
+        % header ("tx_uav_id,value"), others start with data immediately.
+        % Read until a line that looks like a data record, then rewind to it.
+        dataPattern = '^\[\d{4}-\d{2}-\d{2} \d{2}:\d{2}:\d{2}\.\d+\] [-\d]';
+        linePos = ftell(fid);
+        while true
+            line = fgetl(fid);
+            if ~ischar(line)
+                break;  % EOF
+            end
+            if ~isempty(regexp(line, dataPattern, 'once'))
+                fseek(fid, linePos, 'bof');  % rewind to start of this line
+                break;
+            end
+            linePos = ftell(fid);
         end
         data = textscan(fid, '[%26c] %d,%f');
         fclose(fid);
 
-        ts = datetime(data{1}, 'InputFormat', 'yyyy-MM-dd HH:mm:ss.SSSSSS');
+        ts = datetime(cellstr(data{1}), 'InputFormat', 'yyyy-MM-dd HH:mm:ss.SSSSSS');
         txId = int32(data{2});
         val = data{3};
 

aerpaw/results/resultsAnalysis.m

@@ -3,7 +3,8 @@ resultsPath = fullfile(matlab.project.rootProject().RootFolder, "sandbox", "two_
 
 % Plot GPS logged data and scenario information (domain, objective, obstacles)
 seaToGroundLevel = 110; % measured approximately from USGS national map viewer
-[fGlobe, G] = plotGpsLogs(resultsPath, seaToGroundLevel);
+plotWholeFlight = true; % do not attempt to automatically trim initial and final positioning and landing from flight plot (buggy)
+[fGlobe, G] = plotGpsLogs(resultsPath, seaToGroundLevel, true);
 
 % Plot radio statistics
 [fRadio, R] = plotRadioLogs(resultsPath);
@@ -21,7 +22,7 @@ makeVideo = true;
 % Define scenario according to CSV specification
 domain = rectangularPrism;
 domain = domain.initialize([params.domainMin; params.domainMax], REGION_TYPE.DOMAIN, "Domain");
-domain.objective = domain.objective.initialize(objectiveFunctionWrapper(params.objectivePos, reshape(params.objectiveVar, [2 2])), domain, params.discretizationStep, params.protectedRange, params.sensorPerformanceMinimum);
+domain.objective = domain.objective.initialize(objectiveFunctionWrapper(params.objectivePos, reshape(params.objectiveVar, [1, 2 2])), domain, params.discretizationStep, params.protectedRange, params.sensorPerformanceMinimum);
 
 agents = cell(size(params.initialPositions, 2) / 3, 1);
 for ii = 1:size(agents, 1)