DocumentCode :
2293232
Title :
Adaptive polarization for spacecraft communications systems
Author :
Griffin, B.D. ; Haupt, Randy ; Chung, You Chung
Author_Institution :
746 Test Squadron, Holloman AFB, NM, USA
Volume :
2
fYear :
2002
fDate :
2002
Abstract :
Communications antennas on spacecraft are usually circularly polarized. As the spacecraft maneuvers, its antenna and the ground station antenna may not point directly at each other. Antennas not properly aligned for optimal power transfer usually create a polarization mismatch and a loss in transferred power. In this paper, a scheme for compensating for polarization mismatch is considered using crossed dipoles. One of the crossed dipole´s amplitude and phase is adjusted using numerical optimization, and the Numerical Electromagnetic Code generates the electromagnetic response. Optimizing only for circular polarization produces losses in radiated power that offset the polarization correction. The polarization optimization may improve power transferred when the spacing between the orthogonal dipoles is increased. The next step modified the optimization process to consider power transferred. With this improvement, the power transferred always increased up to a maximum of 2.0 dB at θ = 80°. Using adaptive crossed dipoles at the transmitter and receiver was also considered and further improved the model.
Keywords :
adaptive antenna arrays; dipole antenna arrays; electromagnetic wave polarisation; satellite antennas; space vehicles; adaptive crossed dipoles; adaptive polarization; circular polarization; communications antennas; crossed dipoles; electromagnetic response; orthogonal dipoles; polarization mismatch; spacecraft communications systems; Antennas and propagation; Atmospheric modeling; Dipole antennas; Directive antennas; Electromagnetic radiation; Electromagnetic scattering; Electromagnetic wave polarization; Receiving antennas; Satellite antennas; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1035659
Filename :
1035659
Link To Document :
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