Abstract
The problem posed by fiber-optic data links (FODLs) and the approaches used to address them are discussed in the context of subsystem design, modeling, and dynamic flight testing. With respect to FODL kinematics modeling, four regions are defined and the modeling implications discussed: fiber on the bobbin; the near field, around the peel point; transition zone, between the near and far fields; and the far field, extended from the bobbin. The objectives of technology demonstration projects related to command and control of air vehicles are summarized. The potential utility of optical fiber bandwidth as a means for reducing the complexity of expendable missiles by transferring data-processing functions from the missile to the launch platform is discussed. Insights are offered into operational weapon system effectiveness improvements, which can be achieved through the integration of a FODL system.< <ETX xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">></ETX>
Published Version
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