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RunGUI.m
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RunGUI.m
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function varargout = RunGUI(varargin)
% RUNGUI MATLAB code for RunGUI.fig
% RUNGUI, by itself, creates a new RUNGUI or raises the existing
% singleton*.
%
% H = RUNGUI returns the handle to a new RUNGUI or the handle to
% the existing singleton*.
%
% RUNGUI('CALLBACK',hObject,eventData,handles,...) calls the local
% function named CALLBACK in RUNGUI.M with the given input arguments.
%
% RUNGUI('Property','Value',...) creates a new RUNGUI or raises the
% existing singleton*. Starting from the left, property value pairs are
% applied to the GUI before RunGUI_OpeningFcn gets called. An
% unrecognized property name or invalid value makes property application
% stop. All inputs are passed to RunGUI_OpeningFcn via varargin.
%
% *See GUI Options on GUIDE's Tools menu. Choose "GUI allows only one
% instance to run (singleton)".
%
% See also: GUIDE, GUIDATA, GUIHANDLES
% Edit the above text to modify the response to help RunGUI
% Last Modified by GUIDE v2.5 15-Mar-2014 15:06:17
% Begin initialization code - DO NOT EDIT
gui_Singleton = 1;
gui_State = struct('gui_Name', mfilename, ...
'gui_Singleton', gui_Singleton, ...
'gui_OpeningFcn', @RunGUI_OpeningFcn, ...
'gui_OutputFcn', @RunGUI_OutputFcn, ...
'gui_LayoutFcn', [] , ...
'gui_Callback', []);
if nargin && ischar(varargin{1})
gui_State.gui_Callback = str2func(varargin{1});
end
if nargout
[varargout{1:nargout}] = gui_mainfcn(gui_State, varargin{:});
else
gui_mainfcn(gui_State, varargin{:});
end
% End initialization code - DO NOT EDIT
% --- Executes just before RunGUI is made visible.
function RunGUI_OpeningFcn(hObject, eventdata, handles, varargin)
% This function has no output args, see OutputFcn.
% hObject handle to figure
% eventdata reserved - to be defined in a future version of MATLAB
% handles structure with handles and user data (see GUIDATA)
% varargin command line arguments to RunGUI (see VARARGIN)
% Choose default command line output for RunGUI
handles.output = hObject;
% Update handles structure
guidata(hObject, handles);
% UIWAIT makes RunGUI wait for user response (see UIRESUME)
% uiwait(handles.RunGUI);
global ANF_DATA sec_elapsed;
sec_elapsed = 0;
ANF_DATA.Setup.run_HM = 0;
updateAeroFig(handles);
function timerCallback(obj, event, handles)
global sec_elapsed;
if sec_elapsed >= 0
sec_elapsed = sec_elapsed + 1;
% update gui
sec = mod(sec_elapsed, 60);
min = floor(sec_elapsed/60);
set(handles.txtTime, 'String', sprintf('%02i:%02i', min, sec));
drawnow
else
stop(obj);
delete(obj);
end
% --- Outputs from this function are returned to the command line.
function varargout = RunGUI_OutputFcn(hObject, eventdata, handles)
% varargout cell array for returning output args (see VARARGOUT);
% hObject handle to figure
% eventdata reserved - to be defined in a future version of MATLAB
% handles structure with handles and user data (see GUIDATA)
% Get default command line output from handles structure
varargout{1} = handles.output;
% --- Executes on selection change in lstStatus.
function lstStatus_Callback(hObject, eventdata, handles)
% hObject handle to lstStatus (see GCBO)
% eventdata reserved - to be defined in a future version of MATLAB
% handles structure with handles and user data (see GUIDATA)
% Hints: contents = cellstr(get(hObject,'String')) returns lstStatus contents as cell array
% contents{get(hObject,'Value')} returns selected item from lstStatus
% --- Executes during object creation, after setting all properties.
function lstStatus_CreateFcn(hObject, eventdata, handles)
% hObject handle to lstStatus (see GCBO)
% eventdata reserved - to be defined in a future version of MATLAB
% handles empty - handles not created until after all CreateFcns called
% Hint: listbox controls usually have a white background on Windows.
% See ISPC and COMPUTER.
if ispc && isequal(get(hObject,'BackgroundColor'), get(0,'defaultUicontrolBackgroundColor'))
set(hObject,'BackgroundColor','white');
end
% --- Executes on button press in cmdAbort.
function cmdAbort_Callback(hObject, eventdata, handles)
% hObject handle to cmdAbort (see GCBO)
% eventdata reserved - to be defined in a future version of MATLAB
% handles structure with handles and user data (see GUIDATA)
global sec_elapsed ANF_DATA ANF_RESULTS_AIR ANF_RESULTS_GROUND ANF_RESULTS_HM;
if sec_elapsed == 0
%-- run
set(hObject, 'String', 'Abort');
t = timer('Period', 1.0, 'ExecutionMode', 'fixedDelay', 'StartDelay', 1.0);
t.TimerFcn = {@timerCallback, handles};
start(t);
addStatus(handles, 'Analysis started');
% check for geometry
try
formatted_wing_data = fnParseWingData(ANF_DATA.Geometry);
W = fnCalcCG(ANF_DATA);
S = fnCalcPlanformArea(formatted_wing_data);
catch ME
addStatus(handles, 'Aircraft definition incomplete.');
killAnalysis(handles);
end
% check for air data/flight conditions
try
DISA = ANF_DATA.Air.DISA;
hRunway = ANF_DATA.Air.runway_alt;
hCruise = hRunway + ANF_DATA.Air.cruise_height;
rho = fnAtmosphere(hCruise, DISA);
Ve = ANF_DATA.Air.cruise_speed;
CL = W/(1/2*rho*Ve^2*S);
catch ME
addStatus(handles, 'Flight conditions definition incomplete.');
killAnalysis(handles);
end
% execute main code
if isvalid(t) && sec_elapsed>=0
addStatus(handles, 'Running in-air aerodynamics...');
try
ANF_RESULTS_AIR = fnRunAVL(ANF_DATA.Directory, 0, CL, 0, 0, 0, ANF_DATA);
updateAeroFig(handles);
catch ME
addStatus(handles, [ME.identifier ': ' ME.message])
killAnalysis(handles);
end
end
if isvalid(t) && sec_elapsed>=0
addStatus(handles, 'Running ground effect aerodynamics...');
try
ANF_RESULTS_GROUND = fnRunAVL(ANF_DATA.Directory, 1, CL, 0, 0, 0, ANF_DATA);
updateAeroFig(handles);
catch ME
addStatus(handles, [ME.identifier ': ' ME.message])
killAnalysis(handles);
end
end
ANF_RESULTS_HM = [];
if isvalid(t) && sec_elapsed>=0 && ANF_DATA.Setup.run_HM
addStatus(handles, 'Running hinge moment cases...');
if ~isfield(ANF_DATA, 'Interaction') || ~isfield(ANF_DATA.Interaction, 'max_elev')
ANF_DATA.Interaction.max_elev = clDefaults.Interaction_max_elev;
end
if ~isfield(ANF_DATA, 'Interaction') || ~isfield(ANF_DATA.Interaction, 'max_rud')
ANF_DATA.Interaction.max_rud = clDefaults.Interaction_max_rud;
end
if ~isfield(ANF_DATA, 'Interaction') || ~isfield(ANF_DATA.Interaction, 'max_aileron')
ANF_DATA.Interaction.max_aileron = clDefaults.Interaction_max_ail;
end
try
AVLResults = fnRunAVL(ANF_DATA.Directory, 0, CL, ...
ANF_DATA.Interaction.max_elev/180*pi, 0, 0, ANF_DATA);
ANF_RESULTS_HM.elev_dn = AVLResults.hm_elev;
AVLResults = fnRunAVL(ANF_DATA.Directory, 0, CL, ...
-ANF_DATA.Interaction.max_elev/180*pi, 0, 0, ANF_DATA);
ANF_RESULTS_HM.elev_up = AVLResults.hm_elev;
AVLResults = fnRunAVL(ANF_DATA.Directory, 0, CL, ...
0, ANF_DATA.Interaction.max_ail/180*pi, 0, ANF_DATA);
ANF_RESULTS_HM.ail_dn = AVLResults.hm_ail;
AVLResults = fnRunAVL(ANF_DATA.Directory, 0, CL, ...
0, -ANF_DATA.Interaction.max_ail/180*pi, 0, ANF_DATA);
ANF_RESULTS_HM.ail_up = AVLResults.hm_ail;
% vtail is symmetric (should be symmetric)
AVLResults = fnRunAVL(ANF_DATA.Directory, 0, CL, ...
0, 0, ANF_DATA.Interaction.max_rud/180*pi, ANF_DATA);
ANF_RESULTS_HM.rud = AVLResults.hm_rud;
catch ME
addStatus(handles, [ME.identifier ': ' ME.message])
killAnalysis(handles);
end
end
addStatus(handles, 'Analysis finished');
%-- finished execution
% destroy timer object normally
if isvalid(t)
stop(t);
delete(t);
end
resetGUI(handles);
else
% abort
killAnalysis(handles);
end
function addStatus(handles, msg)
status = get(handles.lstStatus, 'String');
status{numel(status)+1} = msg;
set(handles.lstStatus, 'String', status);
function resetGUI(handles)
global sec_elapsed;
sec_elapsed = 0;
set(handles.cmdAbort, 'String', 'Run');
function killAnalysis(handles)
global sec_elapsed;
sec_elapsed = -100;
status = get(handles.lstStatus, 'String');
status{numel(status)+1} = 'Interrupting analysis...';
set(handles.lstStatus, 'String', status);
function txtTime_Callback(hObject, eventdata, handles)
% hObject handle to txtTime (see GCBO)
% eventdata reserved - to be defined in a future version of MATLAB
% handles structure with handles and user data (see GUIDATA)
% Hints: get(hObject,'String') returns contents of txtTime as text
% str2double(get(hObject,'String')) returns contents of txtTime as a double
% --- Executes during object creation, after setting all properties.
function txtTime_CreateFcn(hObject, eventdata, handles)
% hObject handle to txtTime (see GCBO)
% eventdata reserved - to be defined in a future version of MATLAB
% handles empty - handles not created until after all CreateFcns called
% Hint: edit controls usually have a white background on Windows.
% See ISPC and COMPUTER.
if ispc && isequal(get(hObject,'BackgroundColor'), get(0,'defaultUicontrolBackgroundColor'))
set(hObject,'BackgroundColor','white');
end
% --- Executes during object deletion, before destroying properties.
function RunGUI_DeleteFcn(hObject, eventdata, handles)
% hObject handle to RunGUI (see GCBO)
% eventdata reserved - to be defined in a future version of MATLAB
% handles structure with handles and user data (see GUIDATA)
global time_elapsed;
killAnalysis(handles);
clear time_elapsed;
function updateAeroFig(handles)
global ANF_RESULTS_AIR ANF_RESULTS_GROUND ANF_DATA;
cla(handles.figAero, 'reset');
hold(handles.figAero, 'on');
if ~ANF_RESULTS_AIR.NeedUpdate
AoA0 = ANF_RESULTS_AIR.Alpha/180*pi;
CL0 = ANF_RESULTS_AIR.CL;
CLa = ANF_RESULTS_AIR.CLa;
Cm0 = ANF_RESULTS_AIR.Cm;
Cma = ANF_RESULTS_AIR.Cma;
AoA = -5:0.5:16;
CL = (AoA/180*pi-AoA0)*CLa + CL0;
Cm = (AoA/180*pi-AoA0)*Cma + Cm0;
% plot CLmax
if ~isfield(ANF_DATA, 'Air') || ~isfield(ANF_DATA.Air, 'CL_max')
ANF_DATA.Air.CL_max = clDefaults.Air_CL_max;
end
CLmax = ANF_DATA.Air.CL_max;
plot([-5 16], [CLmax CLmax], 'LineStyle', '-.', 'Color', 'r', 'LineWidth', 2);
% plot analysis results
[h_axes l1 l2] = plotyy(AoA, CL, AoA, Cm);
set(l1, 'LineWidth', 2);
set(l2, 'LineWidth', 2);
% labeling
xlabel(handles.figAero, '\alpha (deg)');
ylabel(h_axes(1), 'CL (\delta_{e}=0)');
ylabel(h_axes(2), 'Cm (\delta_{e}=0)');
xlim(h_axes(1), [-5 16]); xlim(h_axes(2), [-5 16]);
ylim(h_axes(1), [0, 2]); ylim(h_axes(2), [-0.25, 0.25]);
set(h_axes(2),'YTick', -0.4:0.1:0.4);
hold(h_axes(1), 'all'); hold(h_axes(2), 'all');
grid on;
legend('CL_{max}','CL','Cm');
end
if ~ANF_RESULTS_GROUND.NeedUpdate
AoA0 = ANF_RESULTS_GROUND.Alpha/180*pi;
CL0 = ANF_RESULTS_GROUND.CL;
CLa = ANF_RESULTS_GROUND.CLa;
Cm0 = ANF_RESULTS_GROUND.Cm;
Cma = ANF_RESULTS_GROUND.Cma;
AoA = -5:0.5:16;
CL = (AoA/180*pi-AoA0)*CLa + CL0;
Cm = (AoA/180*pi-AoA0)*Cma + Cm0;
% plot analysis results
plot(h_axes(1), AoA, CL, 'b--', 'LineWidth', 2);
plot(h_axes(2), AoA, Cm, '--', 'Color',[0 0.5 0], 'LineWidth', 2);
xlim(h_axes(1), [-5 16]); xlim(h_axes(2), [-5 16]);
ylim(h_axes(1), [0, 2]); ylim(h_axes(2), [-0.25, 0.25]);
set(h_axes(1),'YTick', -1:0.25:3);
set(h_axes(2),'YTick', -0.4:0.1:0.4);
grid on;
legend('CL_{max}','CL','CL (Ground)','Cm','Cm (Ground)');
end
hold(handles.figAero, 'off');