diff --git a/unitTests/TestSimulator.m b/unitTests/TestSimulator.m
index 5a628e0e49e042c99c0ea9245938fbc903ea9871..50985ee4434ca41066029f593048af31e5f94cf2 100644
--- a/unitTests/TestSimulator.m
+++ b/unitTests/TestSimulator.m
@@ -1,10 +1,7 @@
classdef TestSimulator < UnitTest
- % TEST FUNZIONANTE, DA RISOLVERE PATH PER simulatorConfig.m in saveTest
- % MANCA refSolid
-
properties
- SimulatorSettings Settings % [-]
+ simulatorSettings Settings
refSimulator
end
@@ -14,13 +11,11 @@ classdef TestSimulator < UnitTest
methods
- function saveTest(testCase, testName, mission)
+ function saveTest(~, testName, mission)
Time = tic;
disp('Started saving simulator tests')
- mainSimPath = fullfile('..', '..', 'simulator');
- addpath(genpath(mainSimPath));
currentPath = fileparts(mfilename('fullpath'));
addpath(genpath(currentPath));
@@ -29,7 +24,7 @@ classdef TestSimulator < UnitTest
wind = WindCustom(mission);
mainSimPath = fullfile('..', 'simulator', 'simulatorConfig.m');
mainOdePath = fullfile('..', 'common', 'settings', 'odeConfig.m');
- SimulatorSettings = Settings(mainSimPath, mainOdePath);
+ SimulatorSettings = Settings(mainSimPath, mainOdePath); %#ok<*PROPLC>
SimulatorSettings.simulator.SMonly = 0;
if strcmp(testName, 'ballistic')
SimulatorSettings.simulator.ballistic = 1;
@@ -75,7 +70,7 @@ classdef TestSimulator < UnitTest
% fieldName = ['referenceState_' verifiable];
testCase.refSimulator = load(filePath, 'stateA', 'stateF');
- testCase.SimulatorSettings = load(filePath, 'SimulatorSettings').SimulatorSettings;
+ testCase.simulatorSettings = load(filePath, 'SimulatorSettings').SimulatorSettings;
% Construct the file path dynamically based on the test parameter
@@ -86,13 +81,13 @@ classdef TestSimulator < UnitTest
methods (Test)
function mainSimulatorTest(testCase, verifiable)
- testCase.createTest(verifiable);
+ testCase.createTestSimulator(verifiable);
mainSimPath = fullfile('..', 'simulator');
addpath(genpath(mainSimPath));
% Run main simulator
- [postp.stateA, postp.stateF] = mainSimulator(testCase.rocket, testCase.wind, testCase.environment, testCase.SimulatorSettings);
+ [postp.stateA, postp.stateF] = mainSimulator(testCase.rocket, testCase.wind, testCase.environment, testCase.simulatorSettings);
postp.stateA = postp.stateA(end, :);
postp.stateF = postp.stateF(end, :);
diff --git a/unitTests/configUnitTest.m b/unitTests/configUnitTest.m
index 4360727fa2a4ba42ffca725cfde0525f119b8e4c..5851157d891ba5bcae6bad4939015162e9efa44a 100644
--- a/unitTests/configUnitTest.m
+++ b/unitTests/configUnitTest.m
@@ -1,7 +1,7 @@
% config unit-test
% choose the mission
-mission = Mission("2024_Lyra_Portugal_October");
+mission = Mission("2025_Orion_Portugal_October");
%% UNIT TESTS TO RUN
% choose which folders to test
diff --git a/unitTests/data/testSimulator/HRE/referenceState_HRE.mat b/unitTests/data/testSimulator/HRE/referenceState_HRE.mat
index 9255c4f66ee7bbcbbe47857e2252751643986fa8..8cfc399f05c2c3dbefd7c133362c86a7cddcba7c 100644
--- a/unitTests/data/testSimulator/HRE/referenceState_HRE.mat
+++ b/unitTests/data/testSimulator/HRE/referenceState_HRE.mat
@@ -1,3 +1,3 @@
version https://git-lfs.github.com/spec/v1
-oid sha256:2696a5102cf8171d2aa2f889a95ce9c5fdfac502d865acf5be43db919fd6c200
-size 51442799
+oid sha256:6b06e877dfda0149f4c9d53923e00b26c8564dcb427fe7f4978cd46ec8b68d12
+size 51436842
diff --git a/unitTests/data/testSimulator/ballistic/referenceState_ballistic.mat b/unitTests/data/testSimulator/ballistic/referenceState_ballistic.mat
index 15af0520edcca8a2f4ad59625997aea0fe6a2bba..9543c5857ef537d7d777bcdc434b7e7e78b79533 100644
--- a/unitTests/data/testSimulator/ballistic/referenceState_ballistic.mat
+++ b/unitTests/data/testSimulator/ballistic/referenceState_ballistic.mat
@@ -1,3 +1,3 @@
version https://git-lfs.github.com/spec/v1
-oid sha256:b82a489c282a3fcf30b5e4ff78fe07216c4e1ed4bcb24b84ffb8ddf7a8f0b7f8
-size 51073079
+oid sha256:946f4c8524c558b73f4d6a53fb920977215b32c220f543137d7a2d4e64c26a14
+size 50932249
diff --git a/unitTests/tests/apogeeUnitTests.m b/unitTests/tests/apogeeUnitTests.m
deleted file mode 100644
index 678ed54488f2dcf21d9400856f2ef1ea51a4f928..0000000000000000000000000000000000000000
--- a/unitTests/tests/apogeeUnitTests.m
+++ /dev/null
@@ -1,114 +0,0 @@
-%{
-apogeeUnitTest - this script is the apogee analysis unit test
-
-CALLED SCRIPTS:
-
-CALLED FUNCTIONS:
-
-CALLED DATA FILES: /data
-
-NOTES: in order to run this script as a test, it has to be called by
-'runtests' funciton. (ex.: results = runtests('apogeeUnitTests')). If you want to
-run it as a simple script, it's advised to active 'pause on errors'.
-
-REVISIONS:
-- 0 31/03/2023, release Matteo Gotti
-- 1 02/04/2023, update Riccardo Cadamuro
- less cases to be tested, different phases added
-
-Copyright © 2021, Skyward Experimental Rocketry, AFD department
-All rights reserved
-
-SPDX-License-Identifier: GPL-3.0-or-later
-
-%}
-
-% tolerance
-toll.absToll = 0.001;
-toll.relToll = 0.001;
-
-errorMsg = 'Results errors are exceeding tolerance';
-
-addpath(genpath('../../commonFunctions'))
-addpath(genpath('../../apogeeAnalysis'))
-
-%% StandardApogeeSolid
-run('../data/testApogeeAnalysis/standardApogee/configSLD.m');
-load('../data/testApogeeAnalysis/standardApogee/referenceSOLID.mat');
-load('../data/testApogeeAnalysis/standardApogee/dataSOLID.mat');
-settings.motors = dataSOLID.motors;
-resTest = standardApogee(settings, dataSOLID.vars);
-
-
-checkMS = checkErrorMSA(dataSOLID.ms, resTest.ms, toll);
-if not(checkMS)
- errorMsg = strcat(errorMsg, ' [ms] ');
-end
-
-checkAPO = checkErrorMSA(refSOLID.apogee, resTest.apogee, toll);
-if not(checkAPO)
- errorMsg = strcat(errorMsg, ' [Apogee] ');
-end
-
-checkVEL = checkErrorMSA(refSOLID.vExit, resTest.vExit, toll);
-if not(checkVEL)
- errorMsg = strcat(errorMsg, ' [vExit] ');
-end
-
-checkACC = checkErrorMSA(refSOLID.maxAcc, resTest.max_a, toll);
-if not(checkACC)
- errorMsg = strcat(errorMsg, ' [max_acc] ');
-end
-check = checkACC&&checkVEL&&checkACC&&checkMS;
-assert(check, errorMsg)
-
-%% StandardApogeeHybrid
-run('../data/testApogeeAnalysis/standardApogee/configHYB.m');
-load('../data/testApogeeAnalysis/standardApogee/referenceHYB.mat');
-load('../data/testApogeeAnalysis/standardApogee/dataHYB.mat');
-settings.motors = dataHYB.motors;
-resTest = standardApogee(settings, dataHYB.vars);
-
-checkMS = checkErrorMSA(dataHYB.ms, resTest.ms, toll);
-if not(checkMS)
- errorMsg = strcat(errorMsg, ' [ms] ');
-end
-
-checkAPO = checkErrorMSA(refHYB.apogee, resTest.apogee, toll);
-if not(checkAPO)
- errorMsg = strcat(errorMsg, ' [Apogee] ');
-end
-
-checkVEL = checkErrorMSA(refHYB.vExit, resTest.vExit, toll);
-if not(checkVEL)
- errorMsg = strcat(errorMsg, ' [vExit] ');
-end
-
-checkACC = checkErrorMSA(refHYB.maxAcc, resTest.max_a, toll);
-if not(checkACC)
- errorMsg = strcat(errorMsg, ' [max_acc] ');
-end
-
-check = checkACC&&checkVEL&&checkACC&&checkMS;
-assert(check, errorMsg)
-
-%% engineCutApogeeAnalysis
-run('../data/testApogeeAnalysis/engineCutApogee/config.m');
-load('../data/testApogeeAnalysis/engineCutApogee/dataEC.mat');
-load('../data/testApogeeAnalysis/engineCutApogee/referenceEC.mat');
-
-settings.motors = dataEC.motors;
-resTest = engineCutApogee(settings, dataEC.vars);
-
-checkTCO = checkErrorMSA(refEC.tCO, resTest.tCO, toll);
-if not(checkTCO)
- errorMsg = strcat(errorMsg, ' [cutoff time] ');
-end
-
-checkAPO = checkErrorMSA(refEC.apogee, resTest.apogee, toll);
-if not(checkAPO)
- errorMsg = strcat(errorMsg, ' [Apogee] ');
-end
-
-check = checkAPO&&checkTCO;
-assert(check, errorMsg);
diff --git a/unitTests/tests/artifacts/results.xml b/unitTests/tests/artifacts/results.xml
deleted file mode 100644
index 331354a0d19291893e8ac54b0733f0f10e537297..0000000000000000000000000000000000000000
--- a/unitTests/tests/artifacts/results.xml
+++ /dev/null
@@ -1,181 +0,0 @@
-<?xml version="1.0" encoding="UTF-8" standalone="no" ?>
-<testsuites>
- <testsuite errors="8" failures="0" name="simulatorUnitTests" skipped="0" tests="10" time="13.0302">
- <testcase classname="simulatorUnitTests" name="StandardSolid" time="3.8148">
- <error>Error occurred in simulatorUnitTests/StandardSolid and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "para".
-
- Error in descentParachute (line 51)
- para = settings.stoch.para;
-
- Error in odearguments (line 92)
- f0 = ode(t0,y0,args{:}); % ODE15I sets args{1} to yp0.
-
- Error in ode113 (line 116)
- odearguments(odeIsFuncHandle, odeTreatAsMFile, solver_name, ode, tspan, y0, options, varargin);
-
- Error in stdRun (line 225)
- [Tp, Yp] = ode113(@descentParachute, [t0p, tf], Y0p, settings.ode.optionspara, settings);
-
- Error in simulatorUnitTests (line 39)
- [~, stateToTestF, ~, stateToTestA] = stdRun(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="StandardHRE_Arb1" time="1.4489">
- <error>Error occurred in simulatorUnitTests/StandardHRE_Arb1 and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "altitudes".
-
- Error in setWindData (line 3)
- s = length(wind.altitudes);
-
- Error in stdRun (line 86)
- settings.wind = setWindData(settings.wind);
-
- Error in simulatorUnitTests (line 58)
- [~, stateToTestF, ~, stateToTestA] = stdRun(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="StandardHRE_Arb2" time="1.2899">
- <error>Error occurred in simulatorUnitTests/StandardHRE_Arb2 and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "altitudes".
-
- Error in setWindData (line 3)
- s = length(wind.altitudes);
-
- Error in stdRun (line 86)
- settings.wind = setWindData(settings.wind);
-
- Error in simulatorUnitTests (line 76)
- [~, stateToTestF, ~, stateToTestA] = stdRun(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="StandardHRE_Arb3" time="1.4571">
- <error>Error occurred in simulatorUnitTests/StandardHRE_Arb3 and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "altitudes".
-
- Error in setWindData (line 3)
- s = length(wind.altitudes);
-
- Error in stdRun (line 86)
- settings.wind = setWindData(settings.wind);
-
- Error in simulatorUnitTests (line 94)
- [~, stateToTestF, ~, stateToTestA] = stdRun(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="test6DOF" time="1.3205">
- <error>Error occurred in simulatorUnitTests/test6DOF and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "altitudes".
-
- Error in setWindData (line 3)
- s = length(wind.altitudes);
-
- Error in stdRun (line 86)
- settings.wind = setWindData(settings.wind);
-
- Error in simulatorUnitTests (line 112)
- [~, stateToTestF] = stdRun(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="ballistic" time="0.85344">
- <error>Error occurred in simulatorUnitTests/ballistic and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "altitudes".
-
- Error in setWindData (line 3)
- s = length(wind.altitudes);
-
- Error in stdRunBal (line 69)
- settings.wind = setWindData(settings.wind);
-
- Error in simulatorUnitTests (line 126)
- [~, stateToTestF] = stdRunBal(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="multipleAB" time="0.90323">
- <error>Error occurred in simulatorUnitTests/multipleAB and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "altitudes".
-
- Error in setWindData (line 3)
- s = length(wind.altitudes);
-
- Error in stdRun (line 86)
- settings.wind = setWindData(settings.wind);
-
- Error in simulatorUnitTests (line 140)
- [~, stateToTestF, ~, stateToTestA] = stdRun(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="engineCutSimulator" time="1.8463">
- <error>Error occurred in simulatorUnitTests/engineCutSimulator and it did not run to completion.
- ---------
- Error ID:
- ---------
- 'MATLAB:nonExistentField'
- --------------
- Error Details:
- --------------
- Unrecognized field name
- "altitudes".
-
- Error in setWindData (line 3)
- s = length(wind.altitudes);
-
- Error in stdRun (line 86)
- settings.wind = setWindData(settings.wind);
-
- Error in simulatorUnitTests (line 158)
- [~, stateToTestF, ~, stateToTestA] = stdRun(settings);</error>
- </testcase>
- <testcase classname="simulatorUnitTests" name="WindInputGenerator" time="0.04655"/>
- <testcase classname="simulatorUnitTests" name="WindVariableGenerator" time="0.04959"/>
- </testsuite>
-</testsuites>
diff --git a/unitTests/tests/checkErrorMSA.m b/unitTests/tests/checkErrorMSA.m
deleted file mode 100644
index ef55400d0e8060e4ff1e264a8115685101a784d1..0000000000000000000000000000000000000000
--- a/unitTests/tests/checkErrorMSA.m
+++ /dev/null
@@ -1,46 +0,0 @@
-function check = checkErrorMSA(reference, test, toll)
-%{
-checkErrorMSA - checks that at least one between the relative and absolute
-error between each elemente of the test and reference array is under the given tolerace
-
-INPUT:
- reference, double [m,k]: reference data
- test , double [m,k]: data to be tested
- toll , struct : contains relToll and absToll to be considered
-
-OUTPUT:
- check: TRUE at least one between the absolute and relative error for each element is
- under the prescribed tolerance, FALSE otherways.
-
-REVISIONS:
-- 0 29/03/2023, release Riccardo Cadamuro
-
-Copyright © 2023, Skyward Experimental Rocketry, AFD department
-All rights reserved
-
-%}
- if numel(reference) ~= numel(test)
- error('Refence array and test array shall contain the same number of elements');
- end
-
- reference = reshape(reference, [1, numel(reference)]);
- test = reshape(test, [1, numel(test)]);
-
- relToll = toll.relToll;
- absToll = toll.absToll;
-
- absErr = abs(reference - test);
- relErr = absErr./reference;
-
- % avoid nan in error computation
- indexZero = (reference == 0);
- relErr(indexZero) = absErr(indexZero);
-
- absCheck = absErr < absToll;
- relCheck = relErr < relToll;
-
- check = true;
- if any(sum([absCheck; relCheck]) == 0)
- check = false;
- end
-end
\ No newline at end of file
diff --git a/unitTests/tests/cmnFnctnUnitTests.m b/unitTests/tests/cmnFnctnUnitTests.m
deleted file mode 100644
index 494e6a1b12510e48aad42e323ff487e91884225f..0000000000000000000000000000000000000000
--- a/unitTests/tests/cmnFnctnUnitTests.m
+++ /dev/null
@@ -1,51 +0,0 @@
-%{
-cmnFnctnUnitTests - this script is the common functions unit test
-
-CALLED SCRIPTS:
-
-CALLED FUNCTIONS:
-
-CALLED DATA FILES: /data
-
-NOTES: in order to run this script as a test, it has to be called by
-'runtests' funciton. (ex.: results = runtests('cmnFnctnUnitTests')). If you want to
-run it as a simple script, it's advised to active 'pause on errors'.
-
-REVISIONS:
-- 0 16/03/2023, release Simone Cimolato
-
-Copyright © 2021, Skyward Experimental Rocketry, AFD department
-All rights reserved
-
-SPDX-License-Identifier: GPL-3.0-or-later
-
-%}
-
-errorMsg = 'Results errors are exceeding tolerance';
-addpath(genpath('../../commonFunctions'))
-
-%% InterpCoeffs
-% config
-run('../data/testCommonFunctions/interpCoeffs/config.m');
-
-% reference
-load('../data/testCommonFunctions/interpCoeffs/coeffsValue.mat');
-load('../data/testCommonFunctions/interpCoeffs/angles.mat');
-
-% interpCoeffs
-[testCoeffsValue, testAngles] = interpCoeffs(t, alpha, M, beta, alt, c, settings);
-check = isequal(testCoeffsValue, referenceCoeffsValue) && isequal(testAngles, referenceAngles);
-assert(check, errorMsg)
-
-%% CreateDissileInput
-% config
-run('../data/testCommonFunctions/createDissileInput/config.m');
-
-% reference
-load('../data/testCommonFunctions/createDissileInput/referenceInputValue.mat');
-
-% createDissileInput
-[testInput] = createDissileInput(settings, vars);
-
-check = isequal(testInput, referenceInput);
-assert(check, errorMsg)
diff --git a/unitTests/tests/optUnitTests.m b/unitTests/tests/optUnitTests.m
deleted file mode 100644
index e966ad35f41632fddc08abddcc2fed8e870e1da2..0000000000000000000000000000000000000000
--- a/unitTests/tests/optUnitTests.m
+++ /dev/null
@@ -1,93 +0,0 @@
-%{
-optUnitTest - this script is the aerodynamicOptimization unit test
-
-CALLED SCRIPTS:
-
-CALLED FUNCTIONS:
-
-CALLED DATA FILES: /data
-
-NOTES: in order to run this script as a test, it has to be called by
-'runtests' funciton. (ex.: results = runtests('optUnitTest')). If you want to
-run it as a simple script, it's advised to active 'pause on errors'.
-
-REVISIONS:
-- 0 16/03/2023, release Simone Cimolato
-
-Copyright © 2021, Skyward Experimental Rocketry, AFD department
-All rights reserved
-
-SPDX-License-Identifier: GPL-3.0-or-later
-
-%}
-
-% reference
-load('../data/testOptimization/singleGARun/refOptGA.mat');
-
-% tolerance
-absErr = 1e-6;
-
-errorMsg = 'Results errors are exceeding tolerance';
-errorMsgSM = 'Error in "XCPcheck"';
-errorMsgApo = 'Error in "optimizationGA"';
-
-addpath(genpath('../../../dissileMatcom'))
-addpath(genpath('../../aerodynamicsOptimization'))
-addpath(genpath('../../commonFunctions'))
-
-%% BoatTailTrueModHaackTrue
-% config
-run('../data/testOptimization/singleGARun/config1.m');
-
-% singleGaRun
-[~, ~, testSingleGA1, testSingleGA2] = singleGArun(lb, ub, input, settings);
-
-check1 = ~(abs(ref.ApoBoatModH - testSingleGA1) >= absErr);
-check2 = abs(testSingleGA2 - ref.CBoatModH)<absErr;
-
-assert(or(check1,check2), errorMsg)
-assert(check1,errorMsgApo)
-assert(check2,errorMsgSM)
-
-%% BoatTailFalseModHaackTrue
-% config
-run('../data/testOptimization/singleGARun/config2.m');
-
-% singleGaRun
-[~, ~, testSingleGA1, testSingleGA2] = singleGArun(lb, ub, input, settings);
-
-check1 = ~(abs(ref.ApoModHOnly - testSingleGA1) >= absErr);
-check2 = abs(testSingleGA2 - ref.CModHOnly)<absErr;
-
-assert(or(check1,check2), errorMsg)
-assert(check1,errorMsgApo)
-assert(check2,errorMsgSM)
-
-%% BoatTailFalseModHaackFalse
-% config
-run('../data/testOptimization/singleGARun/config3.m');
-
-% singleGaRun
-[~, ~, testSingleGA1, testSingleGA2] = singleGArun(lb, ub, input, settings);
-
-check1 = ~(abs(ref.ApoNoBoatNoModH - testSingleGA1) >= absErr);
-check2 = abs(testSingleGA2 - ref.CNoBoatNoModH)<absErr;
-
-assert(or(check1,check2), errorMsg)
-assert(check1,errorMsgApo)
-assert(check2,errorMsgSM)
-
-%% BoatTailTrueModHaackFalse
-% config
-run('../data/testOptimization/singleGARun/config4.m');
-
-% singleGaRun
-[~, ~, testSingleGA1, testSingleGA2] = singleGArun(lb, ub, input, settings);
-
-check1 = ~(abs(ref.ApoBoatOnly - testSingleGA1) >= absErr);
-check2 = abs(testSingleGA2 - ref.CBoatOnly)<absErr;
-
-assert(or(check1,check2), errorMsg)
-assert(check1,errorMsgApo)
-assert(check2,errorMsgSM)
-
diff --git a/unitTests/tests/runTest.m b/unitTests/tests/runTest.m
deleted file mode 100644
index f241a4513b96181e19e3a93d7983ac1352b46eb4..0000000000000000000000000000000000000000
--- a/unitTests/tests/runTest.m
+++ /dev/null
@@ -1,18 +0,0 @@
-% runTests
-
-% import
-import matlab.unittest.TestRunner
-import matlab.unittest.Verbosity
-import matlab.unittest.plugins.XMLPlugin
-
-%
-% tests = {'optUnitTests.m','apogeeUnitTests.m','cmnfnctnUnitTests.m',...
-% 'sensitivityUnitTests.m','simulatorUnitTests.m'};
-tests = {'simulatorUnitTests.m'};
-suite = testsuite(tests);
-[~,~] = mkdir('artifacts');
-runner = TestRunner.withTextOutput('OutputDetail',Verbosity.Detailed);
-runner.addPlugin(XMLPlugin.producingJUnitFormat('artifacts/results.xml'))
-
-results = runner.run(suite);
-assertSuccess(results);
diff --git a/unitTests/tests/sensitivityUnitTests.m b/unitTests/tests/sensitivityUnitTests.m
deleted file mode 100644
index a53b83fec0adeff373e841448fd4374be344f679..0000000000000000000000000000000000000000
--- a/unitTests/tests/sensitivityUnitTests.m
+++ /dev/null
@@ -1,55 +0,0 @@
-%{
-sensitivityUnitTest - this script is the sensitivityAnalysis unit test
-
-CALLED SCRIPTS:
-
-CALLED FUNCTIONS:
-
-CALLED DATA FILES: /data
-
-NOTES: in order to run this script as a test, it has to be called by
-'runtests' funciton. (ex.: results = runtests('simulatorUnitTests')). If you want to
-run it as a simple script, it's advised to active 'pause on errors'.
-
-REVISIONS:
-- 0 29/03/2023, release Riccardo Cadamuro
-
-Copyright © 2023, Skyward Experimental Rocketry, AFD department
-All rights reserved
-
-SPDX-License-Identifier: GPL-3.0-or-later
-%}
-
-% tolerance
-toll.absToll = 0.001;
-toll.relToll = 0.001;
-
-errorMsg = 'Results errors are exceeding tolerance';
-
-addpath(genpath('../../commonFunctions'))
-addpath(genpath('../../sensitivityAnalysis'))
-
-run('../data/testSensitivityAnalysis/config.m');
-
-% loading test data
-load('../data/testSensitivityAnalysis/referenceSensitivity.mat');
-
-%% createParameterTest
-check = isequal(referenceSensitivity.parameters, parameters);
-assert(check, errorMsg);
-
-%% sensitivityApogeeLoopTest
-windMat = referenceSensitivity.windMat;
-modFactor = referenceSensitivity.modFactor;
-finalStateReference = referenceSensitivity.Yend;
-
-finalStateTest = zeros(size(finalStateReference));
-for i = 1:settings.stoch.N
- [settingsM, Q0] = updateSettings(settings, parameters, modFactor(i, :), windMat(i, [7 8 11 9 10 12]) );
- Y0 = [0; 0; 0; 0; 0; 0; 0; 0; 0; Q0];
- data = stochAscentLoop(settingsM, Y0);
- finalStateTest(i, :) = data.state.Y(end, :);
-end
-
-check = checkErrorMSA(finalStateReference, finalStateTest, toll);
-assert(check, errorMsg);
\ No newline at end of file
diff --git a/unitTests/tests/simulatorUnitTests.m b/unitTests/tests/simulatorUnitTests.m
deleted file mode 100644
index 820156d8077758fed1245de38d5ab67389dbf85e..0000000000000000000000000000000000000000
--- a/unitTests/tests/simulatorUnitTests.m
+++ /dev/null
@@ -1,210 +0,0 @@
-%{
-simulatorUnitTest - this script is the simulator unit test
-
-CALLED SCRIPTS:
-
-CALLED FUNCTIONS:
-
-CALLED DATA FILES: /data
-
-NOTES: in order to run this script as a test, it has to be called by
-'runtests' funciton. (ex.: results = runtests('simulatorUnitTests')). If you want to
-run it as a simple script, it's advised to active 'pause on errors'.
-
-REVISIONS:
-- 0 16/03/2023, release Simone Cimolato
-Copyright © 2021, Skyward Experimental Rocketry, AFD department
-All rights reserved
-
-SPDX-License-Identifier: GPL-3.0-or-later
-
-%}
-
-% tolerance
-toll.absToll = 0.001;
-toll.relToll = 0.001;
-
-addpath(genpath('../../commonFunctions'))
-addpath(genpath('../../simulator'))
-
-errorMsg = 'Results errors are exceeding tolerance';
-
-%% StandardSolid
-run('../data/testSimulator/standard_solid/config.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/standard_solid/referenceState_std_solid.mat');
-
-% simulator
-[~, stateToTestF, ~, stateToTestA] = stdRun(settings);
-
-stateToTest.A = stateToTestA(end, :); % state at end of ascent
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-stateToTest.F = [stateToTest.F zeros(1, 7)]; % to avoid problems later in checkErrorSimulator
-
-checkA = checkErrorMSA(referenceState.stateA_std_solid, stateToTest.A, toll);
-checkF = checkErrorMSA(referenceState.stateF_std_solid, stateToTest.F, toll);
-check = checkF && checkA;
-
-assert(check, errorMsg)
-
-%% StandardHRE - arb 1
-run('../data/testSimulator/standard_HRE/config1.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/standard_HRE/referenceState_std_HRE_ARB1.mat');
-
-% simulator
-[~, stateToTestF, ~, stateToTestA] = stdRun(settings);
-
-stateToTest.A = stateToTestA(end, :); % state at end of ascent
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-stateToTest.F = [stateToTest.F zeros(1, 7)]; % to avoid problems later in checkErrorSimulator
-
-checkA = checkErrorMSA(referenceState.stateA_std_HRE, stateToTest.A, toll);
-checkF = checkErrorMSA(referenceState.stateF_std_HRE, stateToTest.F, toll);
-check = checkA && checkF;
-assert(check, errorMsg)
-
-%% StandardHRE - arb 2
-run('../data/testSimulator/standard_HRE/config2.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/standard_HRE/referenceState_std_HRE_ARB2.mat');
-
-% simulator
-[~, stateToTestF, ~, stateToTestA] = stdRun(settings);
-
-stateToTest.A = stateToTestA(end, :); % state at end of ascent
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-stateToTest.F = [stateToTest.F zeros(1, 7)]; % to avoid problems later in checkErrorSimulator
-
-checkA = checkErrorMSA(referenceState.stateA_std_HRE, stateToTest.A, toll);
-checkF = checkErrorMSA(referenceState.stateF_std_HRE, stateToTest.F, toll);
-check = checkA && checkF;
-assert(check, errorMsg)
-
-%% StandardHRE - arb 3
-run('../data/testSimulator/standard_HRE/config3.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/standard_HRE/referenceState_std_HRE_ARB3.mat');
-
-% simulator
-[~, stateToTestF, ~, stateToTestA] = stdRun(settings);
-
-stateToTest.A = stateToTestA(end, :); % state at end of ascent
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-stateToTest.F = [stateToTest.F zeros(1, 7)]; % to avoid problems later in checkErrorSimulator
-
-checkA = checkErrorMSA(referenceState.stateA_std_HRE, stateToTest.A, toll);
-checkF = checkErrorMSA(referenceState.stateF_std_HRE, stateToTest.F, toll);
-check = checkA && checkF;
-assert(check, errorMsg)
-
-%% 6 DOF
-run('../data/testSimulator/6DOF/config.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/6DOF/referenceState6DOF.mat');
-
-% simulator
-[~, stateToTestF] = stdRun(settings);
-
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-
-check = checkErrorMSA(referenceState.stateF6DOF, stateToTest.F, toll);
-assert(check, errorMsg)
-
-%% ballistic
-run('../data/testSimulator/ballistic/config.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/ballistic/referenceStateBallistic.mat');
-
-% simulator
-[~, stateToTestF] = stdRunBal(settings);
-
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-
-check = checkErrorMSA(referenceState.stateFBallistic, stateToTest.F, toll);
-assert(check, errorMsg)
-
-%% multiple AB
-run('../data/testSimulator/multiple_AB/config.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/multiple_AB/referenceState_multipleAB.mat');
-
-% simulator
-[~, stateToTestF, ~, stateToTestA] = stdRun(settings);
-
-stateToTest.A = stateToTestA(end, :); % state at end of ascent
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-stateToTest.F = [stateToTest.F zeros(1, 7)]; % to avoid problems later in checkErrorSimulator
-
-checkA = checkErrorMSA(referenceState.stateA_multipleAB, stateToTest.A, toll);
-checkF = checkErrorMSA(referenceState.stateF_multipleAB, stateToTest.F, toll);
-check = checkF && checkA;
-assert(check, errorMsg)
-
-%% engineCutSimulator
-run('../data/testSimulator/engineCut/config.m');
-
-% loading test data
-referenceState = load('../data/testSimulator/engineCut/referenceState_engineCut.mat');
-
-% simulator
-[~, stateToTestF, ~, stateToTestA] = stdRun(settings);
-
-stateToTest.A = stateToTestA(end, :); % state at end of ascent
-stateToTest.F = stateToTestF(end, :); % final state, at touchdown
-stateToTest.F = [stateToTest.F zeros(1, 7)]; % to avoid problems later in checkErrorSimulator
-
-checkA = checkErrorMSA(referenceState.stateA_engineCut, stateToTest.A, toll);
-checkF = checkErrorMSA(referenceState.stateF_engineCut, stateToTest.F, toll);
-check = checkF && checkA;
-assert(check, errorMsg)
-
-%%% WIND MODELS
-
-%% WindInputGenerator
-settings.wind.inputGround = 6;
-settings.wind.inputAlt = linspace(0, 4000, 100); % altitude vector [m]
-settings.wind.inputMagnitude = [6 * ones(1, 12), 12 * ones(1, 50), 20 * ones(1,38)];
-settings.wind.inputAzimut = 180 * ones(1, 100); % wind azimut angle at each altitude (toward wind incoming direction) [deg]
-settings.wind.inputMult = (settings.wind.inputMagnitude./settings.wind.inputGround - 1) * 100;
-inputUncertainty = [50, 180];
-z = 200;
-
-% loading test data
-referenceState = load('../data/testSimulator/windModels/referenceWindInputComponents.mat');
-
-% wind generation
-[StateToTest.uw, StateToTest.vw, StateToTest.ww] = windInputGenerator(settings, z, inputUncertainty);
-
-check1 = isequal(StateToTest.uw, referenceState.uwInput);
-check2 = isequal(StateToTest.vw, referenceState.vwInput);
-check3 = isequal(StateToTest.ww, referenceState.wwInput);
-check = check1 && check2 && check3;
-assert(check, errorMsg)
-
-%% WindVariableGenerator
-wind.magG = 4.7;
-wind.azG = 75*pi/180;
-wind.hG = 100;
-wind.magH = 13;
-wind.hH = 1000;
-z = 200;
-
-% loading test data
-referenceState = load('../data/testSimulator/windModels/referenceWindVariableComponents.mat');
-
-% wind generation
-[StateToTest.uw, StateToTest.vw, StateToTest.ww] = windVariableGenerator(z, wind);
-
-check1 = isequal(StateToTest.uw, referenceState.uwVariable);
-check2 = isequal(StateToTest.vw, referenceState.vwVariable);
-check3 = isequal(StateToTest.ww, referenceState.wwVariable);
-check = check1 && check2 && check3;
-assert(check, errorMsg)