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  • 1
    Electronic Resource
    Electronic Resource
    [S.l.] : American Institute of Physics (AIP)
    Journal of Applied Physics 78 (1995), S. 6940-6948 
    ISSN: 1089-7550
    Source: AIP Digital Archive
    Topics: Physics
    Notes: A fast approximate method is described to calculate the acoustic scattering from a one-dimensional Dirichlet band-limited fractal surface. The formulation is based on a perturbation of the Green's function allowing an approximation of the propagator in the kernel of the Helmholtz integral equation, which reduces the integral equation to a convolution equation. This allows us to find a solution using Fourier transforms rather than the usual matrix inversion that is required. We have shown that in the limit of small kσ, where k is the incident wave number and σ is the rms height, it is possible to find accurate closed form expressions for the reflection coefficients Rn, the spectral components of the normal gradient of the field ψn, the scattered field psca, and the angular scattering coefficient Isca representing the scattering from a band-limited fractal surface. For small values of kσ(very-much-less-than)1, we have used the generalized Rayleigh method [D. L. Jaggard and X. Sun, J. Appl. Phys. 68, 5456 (1990)] to determine the theoretical linear relationship which exists between the slope of the absolute value of the reflection coefficients in dB versus the reflection mode and the fractal dimension D. This theoretical relationship has been verified by using the Green's function perturbation method. This relationship and an analogous relationship between the scattering coefficient and the scattering angle allows the determination of the fractal dimension D and the rms height σ from the scattering pattern when kσ≤0.2. © 1995 American Institute of Physics.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 1995-12-15
    Print ISSN: 0021-8979
    Electronic ISSN: 1089-7550
    Topics: Physics
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  • 3
    Publication Date: 2013-08-31
    Description: A current thrust in satellite communication systems considers a low-Earth orbiting constellations of satellites for continuous global coverage. Conceptual design studies have been done at the time of this design project by LORAL Aerospace Corporation under the program name GLOBALSTAR and by Motorola under their IRIDIUM program. This design project concentrates on the spacecraft design of the GLOBALSTAR low-Earth orbiting communication system. Overview information on the program was gained through the Federal Communications Commission licensing request. The GLOBALSTAR system consists of 48 operational satellites positioned in a Walker Delta pattern providing global coverage and redundancy. The operational orbit is 1389 km (750 nmi) altitude with eight planes of six satellites each. The orbital planes are spaced 45 deg., and the spacecraft are separated by 60 deg. within the plane. A Delta 2 launch vehicle is used to carry six spacecraft for orbit establishment. Once in orbit, the spacecraft will utilize code-division multiple access (spread spectrum modulation) for digital relay, voice, and radio determination satellite services (RDSS) yielding position determination with accuracy up to 200 meters.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: USRA, Proceedings of the 8th Annual Summer Conference: NASA(USRA Advanced Design Program; p 287-297
    Format: application/pdf
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