DESIGN OF THE GUIDANCE, NAVIGATION AND CONTROL SYSTEM OF A LUNAR LANDER | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 57, Volume 12, ASAT Conference, 29-31 May 2007, May 2007, Page 1-17 PDF (257.18 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.2007.23976 | ||||
 View on SCiNiTO | ||||
| Authors | ||||
| GUGLIERI G.1; PERINO M. A.2; QUAGLIOTTI F.1 | ||||
| 1Politecnico di Torino, Dipartimento di Ingegneria Aeronautica e Spaziale, Torino, Italy. | ||||
| 2Alcatel Alenia Space, Torino, Italy. | ||||
| Abstract | ||||
| ABSTRACT This paper provides the MDLM (Moon Descent Landing Module) Guidance, Navigation and Control system design description as result of the analysis and trade-off performed in the frame of the “Italian Vision for Moon Exploration” studies of the Italian Space Agency (ASI). The preliminary design of the GNC system for the lunar lander was performed following the analysis of mission and the design requisites, the definition of the RCS architecture, the simulation of system performances, and, finally, the hardware and the equipments. | ||||
| Keywords | ||||
| Spacecraft Dynamics; guidance; Navigation and Control; Space Exploration | ||||
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