Analysis of a Distributed Array System for Satellite Acquisition

Orbiting satellites and other spatial vehicles have complex trajectories that can usually be precisely approximated with analytical or numerical trajectory estimation algorithms. However, some scenarios, such as Launch and Early Orbit Phase (LEOP) or critical maneuvers, present greater angular uncer...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems 2017-06, Vol.53 (3), p.1158-1168
Hauptverfasser:	Anton, Alberto, Garcia-Rojo, Isabel, Giron, Alejandro, Morales, Eva, Martinez, Ramon
Format:	Artikel
Sprache:	eng
Schlagworte:	Algorithms Antenna arrays Antennas command (TT&C) Computer simulation Design analysis Design criteria Design engineering digital signal processing direction-of-arrival (DoA) estimation Direction-of-arrival estimation Estimation field-programmable gate array (FPGA) ground stations Launch and Early Orbit Phase (LEOP) launchers Maneuvers Mathematical analysis Mathematical models Matlab Satellite tracking Satellites Space vehicles super-resolution system engineering Telemetry tracking Trajectory analysis Uncertainty weighted subspace fitting (WSF)
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