Weak-signal GNSS navigation could potentially increase the robustness, flexibility and autonomy of the navigation architectures for future lunar exploration missions. GNSS reception during the various phases of such a mission suffers from very low signal levels, partial visibility of the GNSS sources and unfavourable geometry, actually making use of the spill over of the beams around the Earth mask. The objective of a recent ESA study was to evaluate the challenges of such a navigation solution using GPS and future Galileo signals with carrier to noise density ratio levels as low as 10 to 15 dBHz. The inves¬tigated mission phases included transfer orbit, low lunar orbits, lunar ascent and descent as well as surface operation and navigation at the Lagrange points L1 and L2.
Weak GNSS signal navigation for lunar exploration missions / Witternigg, Norbert; Obertaxer, Günther; Schönhuber, Michael; Palmerini, Giovanni Battista; Rodriguez, Filippo; Capponi, Luigi; Soualle, Francis; Floch, Jean Jacques. - ELETTRONICO. - 5:(2015), pp. 3928-3944. (Intervento presentato al convegno 28th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2015 tenutosi a Tampa Convention Center, usa nel 2015).
Weak GNSS signal navigation for lunar exploration missions
PALMERINI, Giovanni Battista;
2015
Abstract
Weak-signal GNSS navigation could potentially increase the robustness, flexibility and autonomy of the navigation architectures for future lunar exploration missions. GNSS reception during the various phases of such a mission suffers from very low signal levels, partial visibility of the GNSS sources and unfavourable geometry, actually making use of the spill over of the beams around the Earth mask. The objective of a recent ESA study was to evaluate the challenges of such a navigation solution using GPS and future Galileo signals with carrier to noise density ratio levels as low as 10 to 15 dBHz. The inves¬tigated mission phases included transfer orbit, low lunar orbits, lunar ascent and descent as well as surface operation and navigation at the Lagrange points L1 and L2.File | Dimensione | Formato | |
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