This paper details the design and analysis of the cislunar optical navigation system being proposed for the Orion Earth-Moon (EM) missions. In particular, it presents the mathematics of the navigation filter. It also presents the sensitivity analysis that has been performed to understand the performance of the proposed system, with particular attention paid to entry flight path angle constraints and the DELTA V performance
Navigation Design and Analysis for the Orion Cislunar Exploration Missions
AAS Guidance and Control Conference ; 2014 ; Breckenridge, CO, United States
2014-01-31
Conference paper
No indication
English
Navigation Design and Analysis for the Orion Cislunar Exploration Missions (AAS 14-095)
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