Title :
Guidance augmentation for reducing uncertainty in vision-based hazard mapping during lunar landing
Author :
Crane, E.S. ; Rock, Stephen M.
Author_Institution :
Dept. of Aeronaut. & Astronaut., Stanford Univ., Stanford, CA, USA
Abstract :
A new guidance augmentation scheme, which generates information-seeking trajectory adjustments, is shown to produce improvements in hazard mapping during autonomous lunar landing. This approach utilizes previously developed techniques for detecting hazard objects from images and an Extended Kalman Filter recursive estimation framework in order to create an occupancy grid representation of the hazards in the landing area. The guidance augmentation is driven by a model-predictive scheme which uses predictions of map entropy and fuel usage in order to generate information-seeking acceleration commands which are combined with the targeting capability of Modified Apollo Guidance. An overview of the algorithmic steps required to adjust the trajectory and predict mapping performance and fuel costs are presented. Hazard maps generated using the online information-seeking trajectory adjustments show significant improvement over un-adjusted trajectories where the hazard image data collected is only incidental.
Keywords :
Kalman filters; aircraft landing guidance; entry, descent and landing (spacecraft); nonlinear filters; predictive control; extended Kalman filter recursive estimation framework; guidance augmentation scheme; hazard object detection; information-seeking trajectory adjustments; lunar landing; model-predictive controller; modified apollo guidance; occupancy grid representation; vision-based hazard mapping; Cameras; Hazards; Robot sensing systems; Rocks; Space vehicles; Trajectory; Uncertainty;
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4673-1812-9
DOI :
10.1109/AERO.2013.6496946