Description and Simulation Results for a GNSS Signal-based Navigation System for a Mission to the Moon
- Paper number
IAC-14,A3,2D,30,x25563
- Author
Mrs. Maria Manzano-Jurado, GMV Aerospace & Defence SAU, Spain
- Coauthor
Ms. Julia Alegre-Rubio, G.M.V. Space and Defence, S.A., Spain
- Coauthor
Mr. Andrea Pellacani, GMV Aerospace & Defence SAU, Spain
- Coauthor
Prof.Dr. Gonzalo Seco-Granados, Universidad Autonoma de Barcelona, Spain
- Coauthor
Prof.Dr. Jose A. Lopez-Salcedo, Universidad Autonoma de Barcelona, Spain
- Coauthor
Mr. Enrique Guerrero, Universidad Autonoma de Barcelona, Spain
- Coauthor
Mr. Alberto Garcia, European Space Agency (ESA), The Netherlands
- Year
2014
- Abstract
In the frame of an ESA activity, the objective of the Moon-GNSS study has been to determine the feasibility using weak-signal GNSS (GPS/Galileo) technology in future lunar exploration missions, to improve the navigation performance in terms of accuracy, cost reduction, robustness and autonomy. During the Moon-GNSS activity, the analysis and the identification of the navigation receiver requirements for the upcoming lunar exploration missions have been performed. An extensive simulation campaign has been carried out to assess the achievable performance (signal acquisition and tracking, raw data accuracy, navigation accuracy and robustness) and to provide with the due inputs for the derivation of the Moon-GNSS navigation receiver requirements. The architecture of the GNSS receiver module has been proposed and designed to achieve the low levels of sensitivity required. It is based on the ESA patented “Double-FFT Method” for an efficient implementation of the high-sensitivity processing. Besides, the synergies between GNSS signal/navigation processing and other navigation sensors have been analyzed, using the state of the art of sensors integration for space missions. A Proof-of-Concept demonstrator of the weak-signal Moon-GNSS navigation has been designed and implemented, showing the main functional and performance capabilities of the Moon-GNSS receiver. A test campaign representative of a real Moon-GNSS mission has been performed, covering all the mission phases representative of the real mission conditions in terms of dynamics and signal disturbances. The main conclusions are that a specifically designed GNSS receiver should be capable of receiving and processing GNSS signals coming from Earth during a lunar mission, and that the resulting GNSS measurements can be hybridized with other navigation sensors to improve the standard navigation performances. Furthermore, GNSS stand-alone navigation should be possible in some phases, allowing a dramatic reduction of the frequency of ground operations. A possible roadmap to eventually bring the Moon-GNSS navigation system into an operational status has been proposed and will be presented.
- Abstract document
- Manuscript document
(absent)