Cleaned up makefile, started presentation

LaTeX/approach.tex

@@ -114,7 +114,7 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=\textwidth]{flowcharts/nlp}
+			\includegraphics[width=\textwidth]{LaTeX/flowcharts/nlp}
 			\caption{A flowchart of the TPBVP Solution Approach}
 			\label{nlp}
 		\end{figure}
@@ -176,7 +176,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=\textwidth]{fig/laguerre_plot}
+				\includegraphics[width=\textwidth]{LaTeX/fig/laguerre_plot}
 				\caption{Example of a natural trajectory propagated via the Laguerre-Conway
 				approach to solving Kepler's Problem}
 				\label{laguerre_plot}
@@ -202,7 +202,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=\textwidth]{fig/spiral_plot}
+				\includegraphics[width=\textwidth]{LaTeX/fig/spiral_plot}
 				\caption{An example trajectory showing that classic continuous-thrust orbit
 				shapes, such as this orbit spiral, are easily achievable using a Sims-Flanagan
 				model}
@@ -320,7 +320,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=\textwidth]{flowcharts/mbh}
+				\includegraphics[width=\textwidth]{LaTeX/flowcharts/mbh}
 				\caption{A flowchart visualizing the steps in the monotonic basin hopping
 				algorithm}
 				\label{mbh_flow}

LaTeX/presentation.tex

@@ -0,0 +1,50 @@
+\documentclass{beamer}
+\usetheme{Luebeck}
+
+\definecolor{color1}{HTML}{3A4040}
+\definecolor{color2}{HTML}{F5F2F8}
+\definecolor{color3}{HTML}{B65D4E}
+\definecolor{color4}{HTML}{B6AD96}
+\definecolor{color5}{HTML}{A96041}
+
+\setbeamercolor*{structure}{bg=color3,fg=color3}
+\setbeamercolor*{palette primary}{fg=color1,bg=color4}
+\setbeamercolor*{palette secondary}{fg=color1,bg=color2}
+\setbeamercolor*{palette tertiary}{fg=color1,bg=color2}
+\setbeamercolor*{palette quaternary}{fg=color1,bg=color3}
+\setbeamercolor{alerted text}{fg=color1,bg=color3}
+\setbeamercolor{titlelike}{bg=color2,fg=color1}
+\setbeamercolor*{titlelike}{bg=color2,fg=color1}
+\setbeamercolor{frametitle}{bg=color1,fg=color2}
+\setbeamercolor{background canvas}{bg=color2,fg=color2}
+
+\title{Designing Optimal Low-Thrust Interplanetary Trajectories}
+\subtitle{Utilizing Monotonic Basin Hopping}
+\author{Richard Connor Johnstone}
+\institute{University of Colorado -- Boulder}
+\date{\today}
+
+\begin{document}
+
+\begin{frame}
+	\titlepage
+\end{frame}
+
+\section{Introduction}
+
+	\begin{frame} \frametitle{First Frame}
+		\begin{itemize}
+			\item Item 1
+			\item Item 2
+		\end{itemize}
+	\end{frame}
+
+\section{Introduction}
+
+\section{Introduction}
+
+\section{Introduction}
+
+\section{Introduction}
+
+\end{document}

LaTeX/results.tex

@@ -128,7 +128,7 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMS_plot}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMS_plot}
 			\caption{Depictions of the faster Earth-Mars-Saturn trajectory found by the
 			algorithm to be most efficient; planetary ephemeris arcs are shown during the phase
 			in which the spacecraft approached them}
@@ -137,7 +137,7 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMS_plot_noplanets}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMS_plot_noplanets}
 			\caption{Another depiction of the EMS trajectory, without the planetary ephemeris
 			arcs}
 			\label{ems_nop}
@@ -156,14 +156,14 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMS_thrust_mag}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMS_thrust_mag}
 			\caption{The magnitude of the unit thrust vector over time for the EMS trajectory}
 			\label{ems_mag}
 		\end{figure}
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMS_thrust_components}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMS_thrust_components}
 			\caption{The inertial x, y, and z components of the unit thrust vector over time for
 			the EMS trajectory}
 			\label{ems_components}
@@ -212,7 +212,7 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMJS_plot}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMJS_plot}
 			\caption{Depictions of the slower Earth-Mars-Jupiter-Saturn trajectory found by the
 			algorithm to be the second most efficient; planetary ephemeris arcs are shown during
 			the phase in which the spacecraft approached them}
@@ -221,7 +221,7 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMJS_plot_noplanets}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMJS_plot_noplanets}
 			\caption{Another depiction of the EMJS trajectory, without the planetary ephemeris
 			arcs}
 			\label{emjs_nop}
@@ -236,14 +236,14 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMJS_thrust_mag}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMJS_thrust_mag}
 			\caption{The magnitude of the unit thrust vector over time for the EMJS trajectory}
 			\label{emjs_mag}
 		\end{figure}
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=0.9\textwidth]{fig/EMJS_thrust_components}
+			\includegraphics[width=0.9\textwidth]{LaTeX/fig/EMJS_thrust_components}
 			\caption{The inertial x, y, and z components of the unit thrust vector over time for
 			the EMJS trajectory}
 			\label{emjs_components}
@@ -304,7 +304,7 @@
 
 		\begin{figure}[H]
 			\centering
-			\includegraphics[width=\textwidth]{fig/c3}
+			\includegraphics[width=\textwidth]{LaTeX/fig/c3}
 			\caption{Plot of Delta IV and Atlas V launch vehicle capabilities as they relate to
 			payload mass \cite{c3capabilities} from Vardaxis, et al, 2007 }
 			\label{c3}

LaTeX/thesis.tex

@@ -1,4 +1,4 @@
-\documentclass[defaultstyle,11pt]{thesis}
+\documentclass[defaultstyle,11pt]{LaTeX/thesis}
 
 \usepackage{graphicx}
 \usepackage{amssymb}
@@ -61,7 +61,7 @@
 
 \begin{document}
 
-	\input macros.tex
+	\input LaTeX/macros.tex
 
 	\input LaTeX/introduction.tex
 
@@ -77,8 +77,6 @@
 
 	\bibliographystyle{plain}
 	\nocite{*}
-	\bibliography{thesis}
-
-	\appendix
+	\bibliography{LaTeX/thesis}
 
 \end{document}

LaTeX/trajectory_design.tex

@@ -37,7 +37,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=0.65\textwidth]{fig/2bp}
+				\includegraphics[width=0.65\textwidth]{LaTeX/fig/2bp}
 				\caption{Figure representing the positions of the bodies relative to each other and
 				the center of mass in the two body problem}
 				\label{2bp_fig}
@@ -148,7 +148,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=0.8\textwidth]{fig/kepler}
+				\includegraphics[width=0.8\textwidth]{LaTeX/fig/kepler}
 				\caption{Geometric representation of auxiliary circle}\label{aux_circ}
 			\end{figure}
 
@@ -297,7 +297,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=0.8\textwidth]{fig/patched_conics}
+				\includegraphics[width=0.8\textwidth]{LaTeX/fig/patched_conics}
 				\caption{Patched Conics Example Figure}
 				\label{patched_conics_fig}
 			\end{figure}
@@ -396,7 +396,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=0.8\textwidth]{fig/flyby}
+				\includegraphics[width=0.8\textwidth]{LaTeX/fig/flyby}
 				\caption{Velocity changes during a gravity assist}
 				\label{grav_assist_fig}
 			\end{figure}
@@ -470,7 +470,7 @@
 
 				\begin{figure}[H]
 					\centering
-					\includegraphics[width=0.8\textwidth]{fig/lamberts}
+					\includegraphics[width=0.8\textwidth]{LaTeX/fig/lamberts}
 					\caption{Visualization of the possible solutions to Lambert's Problem}
 					\label{type1type2}
 				\end{figure}
@@ -587,7 +587,7 @@
 
 				\begin{figure}[H]
 					\centering
-					\includegraphics[width=\textwidth]{fig/porkchop}
+					\includegraphics[width=\textwidth]{LaTeX/fig/porkchop}
 					\caption{A sample porkchop plot of an Earth-Mars transfer}
 					\label{porkchop}
 				\end{figure}
@@ -652,7 +652,7 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=0.6\textwidth]{fig/sft}
+				\includegraphics[width=0.6\textwidth]{LaTeX/fig/sft}
 				\caption{Example of an orbit raising using the Sims-Flanagan Transcription with 7
 				Sub-Trajectories}
 				\label{sft_fig}
@@ -739,14 +739,14 @@
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=\textwidth]{fig/low_efficiency}
+				\includegraphics[width=\textwidth]{LaTeX/fig/low_efficiency}
 				\caption{Graphic of an orbit-raising with a low efficiency cutoff}
 				\label{low_efficiency_fig}
 			\end{figure}
 
 			\begin{figure}[H]
 				\centering
-				\includegraphics[width=\textwidth]{fig/high_efficiency}
+				\includegraphics[width=\textwidth]{LaTeX/fig/high_efficiency}
 				\caption{Graphic of an orbit-raising with a high efficiency cutoff}
 				\label{high_efficiency_fig}
 			\end{figure}

LaTeX/trajectory_optimization.tex

@@ -105,7 +105,7 @@
 
 				\begin{figure}[H]
 					\centering
-					\includegraphics[width=\textwidth]{fig/single_shoot}
+					\includegraphics[width=\textwidth]{LaTeX/fig/single_shoot}
 					\caption{Single shooting over a trajectory arc}
 					\label{single_shoot_fig}
 				\end{figure}
@@ -130,7 +130,7 @@
 
 				\begin{figure}[H]
 					\centering
-					\includegraphics[width=\textwidth]{fig/multiple_shoot}
+					\includegraphics[width=\textwidth]{LaTeX/fig/multiple_shoot}
 					\caption{Visualization of a multiple shooting technique over a trajectory arc}
 					\label{multiple_shoot_fig}
 				\end{figure}