\documentclass{article} %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %TCIDATA{OutputFilter=LATEX.DLL} %TCIDATA{Version=4.00.0.2312} %TCIDATA{Created=Wednesday, November 21, 2001 18:13:53} %TCIDATA{LastRevised=Saturday, December 22, 2001 21:19:24} %TCIDATA{} %TCIDATA{} %TCIDATA{Language=American English} %TCIDATA{CSTFile=40 LaTeX article-NewTimes.cst} \newtheorem{theorem}{Theorem} \RequirePackage{alltimes} \RequirePackage{harvard} \let\cite=\citeasnoun \newtheorem{acknowledgement}[theorem]{Acknowledgement} \newtheorem{algorithm}[theorem]{Algorithm} \newtheorem{axiom}[theorem]{Axiom} \newtheorem{case}[theorem]{Case} \newtheorem{claim}[theorem]{Claim} \newtheorem{conclusion}[theorem]{Conclusion} \newtheorem{condition}[theorem]{Condition} \newtheorem{conjecture}[theorem]{Conjecture} \newtheorem{corollary}[theorem]{Corollary} \newtheorem{criterion}[theorem]{Criterion} \newtheorem{definition}[theorem]{Definition} \newtheorem{example}[theorem]{Example} \newtheorem{exercise}[theorem]{Exercise} \newtheorem{lemma}[theorem]{Lemma} \newtheorem{notation}[theorem]{Notation} \newtheorem{problem}[theorem]{Problem} \newtheorem{proposition}[theorem]{Proposition} \newtheorem{remark}[theorem]{Remark} \newtheorem{solution}[theorem]{Solution} \newtheorem{summary}[theorem]{Summary} \newenvironment{proof}[1][Proof]{\noindent\textbf{#1.} }{\ \rule{0.5em}{0.5em}} \input{tcilatex} \begin{document} \author{Philip A. Viton} \title{A Test of HTML Production in SWP4} \date{\today{}} \maketitle \tableofcontents \section{Econometric Approaches \label{econometric}} Econometric approaches to cost efficiency estimate a parametric cost function and then identify cost efficiency via differences between observed cost and the minimum predicted cost. \ (A second approach is presented in section \ref{dea}) Consider carrier $k$ in year $t$. It has a $V$-vector $% \mathbf{z}_{kt}=(z_{kt1},\dots ,z_{ktV})$ of system characteristics and produces the $M$-vector of outputs $\mathbf{y}_{kt}=(y_{kt1},\dots ,y_{ktM})$ from the $N$-vector of inputs $\mathbf{x}_{kt}=(x_{kt1},\dots ,x_{ktN})$ according to the transformation function $f(\mathbf{y}_{kt},\mathbf{x}_{kt};% \mathbf{z}_{kt})=0.$ It is assumed to face the $N$ factor prices $\mathbf{w}% _{kt}=(w_{kt1},\dots ,w_{ktN}).$ \ Its (minimum) cost function $C^{\ast }(% \mathbf{y}_{kt},\mathbf{w}_{kt};\mathbf{z}_{kt})$ is the indirect objective function of the problem: choose inputs $\mathbf{x}_{kt}$ to minimize cost subject to $f$ (the production function), ie: \[ \begin{array}{cc} \text{\textrm{minimize}} & \sum_{n}w_{ktn}x_{ktn} \\ \text{\textrm{subject to:}} & f(\mathbf{y}_{kt},\mathbf{x}_{kt};\mathbf{z}% _{kt})=0.% \end{array}% \]% If $C_{kt}$ is the \emph{observed} cost of carrier $k$ in year $t$, we allow for a failure to attain the minimum cost by writing \begin{equation} C_{kt}=C^{\ast }(\mathbf{y}_{kt},\mathbf{w}_{kt};\mathbf{z}% _{kt})e^{\varepsilon _{kt}} \label{costfn} \end{equation}% where $\varepsilon _{kt}$ is a random variable, so that \begin{equation} \ln C_{kt}=\ln C^{\ast }(\mathbf{y}_{kt},\mathbf{w}_{kt};\mathbf{z}% _{kt})+\varepsilon _{kt} \label{linear} \end{equation} Because the observed cost $C_{kt}$ cannot exceed the theoretical minimum cost $C_{kt}^{\ast },$ $\varepsilon _{kt}$ is necessarily non-negative. \ We obtain a parametric cost function by specifying a functional form for $% C^{\ast }(\mathbf{y}_{kt},\mathbf{w}_{kt};\mathbf{z}_{kt}).$ \ For the remainder of this section, we shall assume that the cost function is translog in inputs and outputs; but that system characteristics enter linearly.\footnote{% Cobb-Douglas models, which are nested sub-models of the translog, were also estimated. \ In all cases they were rejected in favor of the translog.} \ Then we may write equation (\ref{linear}) as: \begin{eqnarray} \ln C^{\ast }(\mathbf{y}_{kt},\mathbf{x}_{kt};\mathbf{z}_{kt}) &=&\alpha _{0}+\sum_{i=1}^{V}\alpha _{i}z_{kti}+\sum_{n=1}^{N}\beta _{n}\ln y_{ktn}+\sum_{m=1}^{M}\gamma _{m}\ln w_{ktm} \label{translog} \\ &&+\frac{1}{2}\sum_{n=1}^{N}\sum_{p=1}^{N}\delta _{np}\ln y_{ktn}\ln y_{ktp}+% \frac{1}{2}\sum_{m=1}^{M}\,\sum_{j=1}^{M}\theta _{mj}\ln w_{ktm}\ln w_{ktj} \nonumber \\ &&+\frac{1}{2}\sum_{n=1}^{N}\sum_{m=1}^{M}\xi _{nm}\ln w_{ktn}\ln w_{ktm} \nonumber \end{eqnarray}% The theory of cost minimization implies that $C^{\ast }(\mathbf{y}_{kt},% \mathbf{w}_{kt};\mathbf{z}_{kt})$ is homogeneous of degree zero in input prices, which places restrictions on the parameters of the cost function (see, eg, \cite{spady-friedlaender:78}); in addition the parameters $\delta ,\theta $ and $\xi $ are symmetric, so that, for example $\delta _{np}=\delta _{pn}.$ \section{The DEA Approach \label{dea}} Data Envelopment Analysis, or DEA, see, eg \cite{bcc:84}, or \cite{fgl:94}, begins by constructing the set of feasible input-output combinations. \ (Another approach was presented in section \ref{econometric}) It then finds, with reference to that set, the input bundle that minimizes the cost of producing the observed output. DEA is non-parametric in that it makes no assumption about the structure of the cost function ---\ indeed it does not explicitly obtain the cost function at all ---\ and, being non-statistical, it has no need for parametric distributional assumptions.\footnote{% This is not to say that DEA cannot be given a statistical foundation: for example, \cite{banker:93} shows that the DEA solution can be considered the maximum-likelihood estimator of a non-parametric monotone increasing and concave production frontier.} To construct the feasible set it begins by assuming that the observed input-output combinations (the data) are feasible and then adds unobserved combinations by considerations of additivity (scale) and disposal.\footnote{% Feasibility of the observed data is not a completely innocuous assumption. If, for example, there are measurement errors, then the observed data may not in fact be feasible.} The upshot is that cost-minimizing carrier selects an input bundle $\mathbf{% \tilde{x}}_{kt}$ to minimize total cost, $\sum_{n}\tilde{x}_{ktn}w_{ktn}=% \mathbf{\tilde{x}}_{kt}^{\prime }\mathbf{w}_{kt}$ subject to feasibility; and this is the solution to the non-linear program \begin{eqnarray*} \text{\textrm{minimize} } &&\sum\nolimits_{n}\tilde{x}_{ktn}w_{ktn} \\ \text{subject to} &\text{:}& \\ \text{\textrm{\ }}\mathbf{y}_{ktm} &=&\mu \sum\nolimits_{l,s}r_{ls}\mathbf{y}% _{lsm}\quad \forall m=1,2,\dots ,M \\ \lambda \mathbf{\tilde{x}}_{ktn} &=&\sum\nolimits_{l,st}r_{ls}\mathbf{x}% _{lsn}\quad \forall n=1,2,\dots ,N \\ \sum\nolimits_{l,s}r_{ls} &=&1 \\ 0 &<&\lambda \leq 1 \\ 0 &<&\mu \leq 1 \end{eqnarray*}% and we define the cost-efficiency of carrier $k$ at period $t$ by \[ \mathrm{CE}_{kt}=\frac{\mathbf{w}_{kt}^{\prime }\mathbf{\tilde{x}}_{kt}}{% \mathbf{w}_{kt}^{\prime }\mathbf{x}_{kt}} \]% the ratio of observed to minimal cost. \ \bibliographystyle{AERNOB} \bibliography{pav} \end{document}