1997 IEEE Aerospace Conference Proceedings, Volumes 1-4These proceedings present innovative aerospace systems and their principal component, the satellite system. The papers highlight the effects of trade-offs caused by the limited resources due to the relative weight, size and power restrictions within a satellite on design choice for computing, programming, sensing and communications within aerospace applications. |
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ACSR Aerospace aircraft algorithm analysis angle antenna aperture applications approach architecture array band bandwidth battery Beowulf bistatic Center checkpoint chip clutter command components cost density distributed distributed shared memory DRAM efficiency energy Engineering fault injection flight frequency function geometry gimbal GMTI GN&C grazing angle hardware IEEE illuminator implemented infrared input integration interface Laboratory matched filter measurements memory mission MLPNN moving target NASA near-field node operations optical orbit output parallel parameters petaflops petaflops computing phase pixels platform processor radar radar cross section radiation range real-time receiver requirements Rome Laboratory satellite SBR Mass Sensitivity scan sensor shown in Figure signal simulation solar cells space spacecraft storage subsystem superconductor surface surveillance Table TeBaD techniques thermal tion track vector workstation