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Eva Smeets added file Chapters/AppendixTrade31.tex
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diff --git a/Chapters/AppendixRefAC.tex b/Chapters/AppendixRefAC.tex
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\newgeometry{top=-0.5cm,bottom=1.4cm}
\chapter{Reference Aircraft}
\label{app:RefAC}
\begin{table}[b!]
\centering
\caption{Non-electric reference aircraft with their corresponding parameters}
\begin{sideways}
\resizebox{0.85\textheight}{!}{%
\begin{tabular}{r|rr|rrrrrrrrrrrrrr|r}
\toprule
\textbf{Category} & \textbf{Type} & \textbf{Engine type} & $\mathbf{EW\,[kg]}$ & $\mathbf{MTOW\,[kg]}$ & $\mathbf{W_{en} \,[kg]}$ & $\mathbf{EW-W_{en}\,[kg]}$ & $\mathbf{P_{br}\,[kW]}$ & $\mathbf{\frac{W}{P}\,\left[\frac{N}{W}\right]}$ & $\mathbf{\frac{W}{S}\,\left[\frac{N}{m^2}\right]}$ & $\mathbf{b\,[m]}$ & $\mathbf{S\,[m^2]}$ & $\mathbf{V_{stall}\,\left[\frac{m}{s}\right]}$ & $\mathbf{C_{L_{max}}\,[-]}$ & $\mathbf{A\,[-]}$ & $\mathbf{s_{TO}\,[m]}$ & $\mathbf{TOP\,\left[\frac{Ns}{m^3}\right]}$ & \textbf{Source} \\
\toprule
Aerobatic & Cap 10C & AEIO-360-B2F & 540 & 780 & 125 & 415 & 134 & 0.057 & 705.3 & 8.08 & 10.85 & 27.5 & 1.52 & 6.0 & 395 & 26.5 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Extra EA-300L & AEIO-540-L1B5 & 672 & 820 & 204 & 468 & 224 & 0.036 & 751.4 & 8.00 & 10.70 & 28.3 & 1.53 & 6.0 & 248 & 17.7 & \cite{Janes} \\
Aerobatic & Extra EA-300S & AEIO-540-L1B5 & 585 & 820 & 204 & 381 & 224 & 0.036 & 820.1 & 7.50 & 9.81 & 30.6 & 1.43 & 5.7 & 248 & 20.6 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Aviat Pitts S-2C & AEIO-540-D4A5 & 524 & 771 & 175 & 349 & 194 & 0.043 & 641.0 & 6.10 & 11.80 & 28.8 & 1.26 & 3.2 & 366 & 22.0 & \cite{Janes} \\
Aerobatic & Zivko Edge 540 & IO-540 & 531 & 703 & 216 & 316 & 254 & 0.032 & 757.3 & 7.42 & 9.10 & 26.4 & 1.78 & 6.1 & 90 & 13.5 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Nemesis NXT & TIO-540-NXT & 726 & 1179 & 181 & 545 & 261 & 0.044 & 1778.6 & 7.32 & 6.50 & 40.8 & 1.74 & 8.2 & 762 & 45.3 & \cite{Janes} \\
Aerobatic & XtremeAir XA-42 & AEIO-580-B1A & 610 & 850 & 204 & 406 & 235 & 0.032 & 741.6 & 7.50 & 11.25 & 27.5 & 1.60 & 5.0 & 400 & 14.8 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Slick 360 & AEIO-360 & 465 & 625 & 127 & 338 & 161 & 0.032 & 659.2 & 7.31 & 8.60 & 28.9 & 1.39 & 6.2 & 351 & 15.0 & \cite{Janes} \\
Aerobatic & Slick 540 & AEIO-540 & 550 & 716 & 204 & 346 & 221 & 0.032 & 814.2 & 7.31 & 8.60 & 30.6 & 1.43 & 6.2 & 351 & 18.3 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Sukhoi Su-31T & Vedeneyev M14P & 750 & 1050 & 214 & 536 & 294 & 0.032 & 804.4 & 7.80 & 11.83 & 29.4 & 1.64 & 5.1 & 110 & 15.6 & \cite{Janes} \\
Kit & GlasAir III & IO-540-K1H5 & 737 & 1098 & 199 & 538 & 224 & 0.048 & 1413.6 & 7.11 & 7.60 & 35.0 & 1.89 & 6.7 & 275 & 35.8 & \cite{Janes} \\
\rowcolor{grey} Kit & Van's RV14 & IO-390 & 562 & 862 & 140 & 422 & 157 & 0.058 & 778.9 & 8.23 & 11.70 & 23.3 & 2.17 & 5.8 & 161 & 20.9 & \cite{Janes} \\
Kit & Van's RV10 & IO-540 & 726 & 1225 & 188 & 538 & 194 & 0.062 & 874.1 & 9.68 & 13.70 & 28.3 & 1.78 & 6.8 & 153 & 30.4 & \cite{Janes} \\
\rowcolor{grey} Kit & Van's RV7 & IO-360 & 505 & 816 & 147 & 359 & 149 & 0.054 & 718.1 & 7.62 & 11.10 & 26.4 & 1.69 & 5.2 & 153 & 22.8 & \cite{Janes} \\
Aerobatic & Grob G 120A & AEIO-540-D4D5 & 1080 & 1440 & 175 & 905 & 194 & 0.075 & 1098.7 & 10.18 & 13.30 & 28.3 & 2.16 & 7.8 & 654 & 38.3 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & General Avia F.22 & O-320-D2A & 582 & 850 & 127 & 455 & 119 & 0.035 & 770.7 & 8.50 & 10.82 & 36.0 & 0.97 & 6.7 & 400 & 27.8 & \cite{GeneralAvia} \\
Aerobatic & Yakovlev Yak-54 & VOKBM M-14P & 769 & 901 & 214 & 555 & 265 & 0.037 & 753.4 & 8.15 & 12.89 & 29.0 & 1.33 & 5.2 & 170 & 20.8 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Laser Z-300 & IO-540 & 522 & 658 & 213 & 309 & 224 & 0.029 & 694.3 & 7.62 & 9.29 & 25.9 & 1.69 & 6.3 & 300 & 11.8 & \cite{York} \\
Aerobatic & Peña Joker & O-235 & 520 & 700 & 113 & 407 & 75 & 0.029 & 660.0 & 8.00 & 10.40 & 22.2 & 2.19 & 6.2 & - & 8.7 & \cite{PenaJoker} \\
\rowcolor{grey} Aerobatic & Mü30 Schlacro & AEIO-540 & 748 & 1050 & 199 & 549 & 223 & 0.043 & 861.2 & 9.00 & 11.96 & 36.0 & 1.08 & 6.5 & - & 34.3 & \cite{Janes} \\
Aerobatic & Zlin Z-50 & AEIO-540-D4B5 & 570 & 720 & 204 & 366 & 194 & 0.04 & 565.1 & 8.58 & 12.50 & 27.2 & 1.24 & 5.9 & - & 18.4 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & MXS-R & IO-540-E & 572 & 835 & 181 & 391 & 194 & 0.047 & 864.1 & 7.32 & 9.48 & 29.8 & 1.58 & 5.7 & - & 25.6 & \cite{Janes} \\
Aerobatic & Mylius MY-103/200 & IO-360 & 620 & 950 & 136 & 484 & 149 & 0.063 & 891.8 & 8.65 & 10.45 & 31.4 & 1.48 & 7.2 & - & 37.8 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Extra EA-200 & AEIO-360-A1E & 562 & 700 & 137 & 426 & 149 & 0.046 & 657.5 & 7.50 & 10.44 & 30.6 & 1.15 & 5.4 & - & 26.3 & \cite{Janes} \\
Kit & Altitude Radial Rocket & VOKBM M-14P & 748 & 1157 & 214 & 534 & 265 & 0.048 & 1351.2 & 7.77 & 8.40 & 38.1 & 1.52 & 7.2 & - & 42.2 & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Yakovlev Yak-55M & VOKBM M-14P & 645 & 840 & 214 & 431 & 265 & 0.035 & 643.8 & 8.10 & 12.80 & 30.6 & 1.13 & 5.1 & - & 19.8 & \cite{Janes} \\
Aerobatic & Dyn'Aero CR100 & AEIO-360-B2F & 550 & 760 & 125 & 425 & 134 & 0.056 & 701.4 & 8.50 & 10.65 & - & - & 6.8 & 351 & - & \cite{Janes} \\
\rowcolor{grey} Aerobatic & Corvus CA-41 540 & TIO-540-U & 545 & 685 & 263 & 282 & 257 & 0.029 & 746.7 & 7.40 & 9.00 & 26.4 & 1.75 & 6.1 & - & - & \cite{Janes} \\
Aerobatic & RUD RA-2 & AEIO-540 [315hp] & 612 & 855 & 204 & 408 & 235 & 0.036 & - & 7.32 & - & 28.3 & - & - & 351 & - & \cite{Janes} \\
\rowcolor{grey} Aerobatic & RUD RA-3 & IO-360 [180hp] & 499 & 816 & 136 & 363 & 134 & 0.06 & - & 7.32 & - & 25.8 & - & - & 351 & - & \cite{Janes} \\
Aerobatic & Terzi T30C Katana & IO-540 [300hp] & 658 & 880 & 213 & 445 & 224 & 0.043 & - & 7.57 & - & - & - & - & - & - & \cite{Katana} \\
\midrule
\multicolumn{3}{r|}{\textit{\textbf{Averages}}} & 622 & 875 & 180 & 442 & 201 & 0.044 & 839.9 & 7.89 & 10.55 & 29.6 & 1.56 & 6.1 & 316 & 24.3 & \\
\bottomrule
\end{tabular}%
}
\end{sideways}
\label{tab:referenceAC}
\end{table}
\restoregeometry
diff --git a/Chapters/AppendixTrade31.tex b/Chapters/AppendixTrade31.tex
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\chapter{AHP Numbers and Results Final Trade-Off}
\label{app:AHP_results2}
%Please do not forget to add new symbols to the nomenclature e.g.: \nomenclature{$t_{element}$}{Thickness coefficient of plate \nomunit{[$-$]}}
\newcolumntype{a}{X}
\newcolumntype{f}{>{\centering\arraybackslash}>{\hsize=.6\hsize}X}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison to determine main criteria weights}
\label{tab:criteriacomparison_3}
\centering
\begin{tabularx}{\textwidth}{a| ffffffff}
\toprule
\textbf{Criterion} & \textbf{A} & \textbf{B} & \textbf{C} & \textbf{D} & \textbf{E} & \textbf{F} & \textbf{G} & \textbf{H} \\
\toprule
\textbf{A} & 1 &1/1.5& 2 & 2 & 3 & 3 & 3.5 & 2.5 \\
\textbf{B} & 1.5 & 1 & 4.5 & 2.5 & 4 & 4 & 5 & 3.5 \\
\textbf{C} & 1/2 &1/4.5& 1 & 1.5 & 2 & 2.5 & 3 & 2 \\
\textbf{D} & 1/2 &1/2.5&1/1.5& 1 & 2 & 2.5 & 2.5 & 2 \\
\textbf{E} & 1/3 & 1/4 & 1/2 & 1/2 & 1 & 1.5 & 2 & 1.5 \\
\textbf{F} & 1/3 & 1/4 &1/2.5&1/2.5& 1/3 & 1 & 1.5 & 1/3 \\
\textbf{G} &1/3.5&1/5.5& 1/3 &1/2.5& 5 &1/1.5& 1 & 1/3 \\
\textbf{H} &1/2.5&1/3.5& 1/2 & 1/2 & 1/3 & 1.5 & 1.5 & 2 \\
\bottomrule
\end{tabularx}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison to determine main criteria weights}
\label{tab:criteriacomparison_4}
\begin{tabular}{lcc}
\toprule
\textbf{Criterion}&\textbf{C1} &\textbf{C2} \\
\toprule
\textbf{C1}& 1 & 3 \\
\textbf{C2}&1/3& 1 \\
\bottomrule
\end{tabular}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison of the options for L/D}
\label{tab:comp_ld}
\begin{tabular}{lccc p{20pt} l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard}
&&\textbf{Ranking}\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 & 4 &1/1.8&&0.3538\\
\textbf{Bi-plane} & 1/4 & 1 &1/4.5&&0.1041\\
\textbf{Canard} & 1.8 & 4.5 & 1 &&0.5421\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
\begin{table}
\centering
\caption{Pairwise comparison of the options for high G turns}
\label{tab:comp_G}
\begin{tabular}{lccc p{20pt}l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard}&&\textbf{Ranking} \\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 &1/1.5& 1/2 &&0.2212\\
\textbf{Bi-plane} & 1.5 & 1 &1/1.5&&0.3189\\
\textbf{Canard} & 2 & 1.5 & 1 &&0.4599\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison of the options for complexity}
\label{tab:comp_comp}
\begin{tabular}{lccc p{20pt}l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard} &&\textbf{Ranking}\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 & 1.5 & 2 &&0.4599\\
\textbf{Bi-plane} &1/1.5& 1 & 1.5 &&0.3189\\
\textbf{Canard} & 1/2 &1/1.5& 1 &&0.2212\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison of the options for propulsive efficiency}
\label{tab:comp_pe}
\begin{tabular}{lccc p{20pt}l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard} &&\textbf{Ranking}\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 & 1 &1/1.5&&0.2857\\
\textbf{Bi-plane} & 1 & 1 &1/1.5&&0.2857\\
\textbf{Canard} & 1.5 & 1.5 & 1 &&0.4286\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison of the options for visibility}
\label{tab:comp_vis}
\begin{tabular}{lccc p{20pt}l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard} &&\textbf{Ranking}\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 & 3 & 1.5 && 0.5000 \\
\textbf{Bi-plane} & 1/3 & 1 & 1/2 && 0.1667\\
\textbf{Canard} &1/1.5& 2 & 1 && 0.3333\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison of the options for safety}
\label{tab:comp_safe}
\begin{tabular}{lccc p{20pt}l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard} &&\textbf{Ranking}\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 & 3 & 1 &&0.4286\\
\textbf{Bi-plane} & 1/3 & 1 & 1/3 &&0.1429\\
\textbf{Canard} & 1 & 3 & 1 &&0.4286\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison of the options for takeoff and landing characteristics}
\label{tab:comp_tol}
\begin{tabular}{lccc p{20pt}l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard} &&\textbf{Ranking}\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 & 1/2 & 2.5 &&0.3172\\
\textbf{Bi-plane} & 2 & 1 & 3 &&0.5217\\
\textbf{Canard} &1/2.5& 1/3 & 1 &&0.1511\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
\begin{table}[htbp]
\centering
\caption{Pairwise comparison of the options for uncertainty of design}
\label{tab:comp_uncertain}
\begin{tabular}{lccc p{20pt}l}
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Design Option} & \textbf{Conventional} & \textbf{Bi-plane} & \textbf{Canard} &&\textbf{Ranking}\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\textbf{Conventional} & 1 & 4 & 2 &&0.5662\\
\textbf{Bi-plane} & 1/4 & 1 & 2 &&0.2416\\
\textbf{Canard} & 1/2 & 1/2 & 1 &&0.1922\\
\cmidrule[0.08em]{1-4} \cmidrule[0.08em]{6-6}
\end{tabular}
\end{table}
