Abstract Lunar final approach navigation is critical for pin-point lunar landing in future missions. This study investigates the use of lunar gravity gradient measurements for autonomous navigation of a lunar probe during the final approach phase. As the spacecraft approaches the Moon, the strength of gravity gradient signals improves. A spaceborne gravity gradiometer can precisely measure local gravity gradients, and the latest lunar gravity model GL1500E is used to provide reference values. The employed truncation degree and order of the gravity model are increased stepwise considering the decreasing altitude of the spacecraft in order to reach a compromise between computational costs and model accuracy. An iterative Kalman filter is developed for coupled orbit and attitude estimation using gravity gradient measurements and attitude quaternions obtained from star sensors. A simulated spacecraft with a gradiometer noise level of 0.01 E is considered. Simulation results show that the spacecraft’s position converges rapidly and achieves an accuracy of less than 100 m at the last epoch.
Autonomous navigation for lunar final approach based on gravity gradient measurements
Advances in Space Research ; 71 , 3 ; 1769-1783
2022-09-27
15 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Autonomous Optical Lunar Navigation
NTRS | 2009
|Autonomous navigation for lunar transfer
AIAA | 1995
|Proposed Autonomous Lunar Navigation System
British Library Conference Proceedings | 1993
|Autonomous navigation using lunar beacons
NTRS | 1983
|