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contributor authorDaigle, Matthew
contributor authorSankararaman, Shankar
date accessioned2017-11-25T07:16:29Z
date available2017-11-25T07:16:29Z
date copyright2016/08/19
date issued2016
identifier issn2332-9017
identifier otherrisk__0_041001.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4234041
description abstractThe operations of a planetary rover depend critically upon the amount of power that can be delivered by its batteries. In order to plan the future operation, it is important to make reliable predictions regarding the end-of-discharge (EOD) time, which can be used to estimate the remaining driving time (RDT) and remaining driving distance (RDD). These quantities are stochastic in nature, not only because there are several sources of uncertainty that affect the rover’s operation but also since the future operating conditions cannot be known precisely. This paper presents a computational methodology to predict these stochastic quantities, based on a model of the rover and its batteries. We utilize a model-based prognostics framework that characterizes and incorporates the various sources of uncertainty into these predictions, thereby assisting operational decision-making. We consider two different types of driving scenarios and develop methods for each to characterize the associated uncertainty. Monte Carlo sampling and the inverse first-order reliability method are used to compute the stochastic predictions of EOD time, RDT, and RDD.
publisherThe American Society of Mechanical Engineers (ASME)
titlePredicting Remaining Driving Time and Distance of a Planetary Rover Under Uncertainty
typeJournal Paper
journal volume2
journal issue4
journal titleASCE-ASME Journal of Risk and Uncertainty in Engineering Systems, Part B: Mechanical Engineering
identifier doi10.1115/1.4032848
journal fristpage41001
journal lastpage041001-11
treeASCE-ASME Journal of Risk and Uncertainty in Engineering Systems, Part B: Mechanical Engineering:;2016:;volume( 002 ):;issue: 004
contenttypeFulltext


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