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Keeping a satellite aloft: two finite fuel stochastic control models

Part of: Stochastic systems and control Stochastic analysis

Published online by Cambridge University Press:  14 July 2016

S. D. Jacka
S. D. Jacka*
Affiliation:
University of Warwick
*
∗Postal address: Department of Statistics, University of Warwick, Coventry CV4 7AL, UK. Email address: s.d.jacka@warwick.ac.uk.
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Abstract

We consider two models for the control of a satellite–in the first, fuel is expended in a linear fashion to move a satellite following a diffusion–where the aim is to keep the satellite above a critical level for as long as possible (or indeed to reach a higher, ‘safe’ level). Under suitable assumptions for the drift and diffusion coefficients, it is shown that the stochastic maximum of the time to fall below the critical level is attained by a policy which imposes a reflecting boundary at the critical level until the fuel is exhausted and jumps the satellite directly to the safe level if this is ever possible. In the second model, there is a nonlinear response to the expenditure of fuel, and no safe level. It is shown that the optimal policy for maximizing the expected discounted time for the satellite to crash is similar, in that equal packets of fuel are used to jump the satellite upwards each time it reaches the critical level.

Keywords

Stochastic controldiffusionstrong maximum principlefinite-fuel problemtotal positivity

MSC classification

Primary: 93E20: Optimal stochastic control
Secondary: 60H30: Applications of stochastic analysis (to PDE, etc.)
Type
Research Papers
Information
Journal of Applied Probability , Volume 36 , Issue 1 , March 1999 , pp. 1 - 20
Copyright
Copyright © Applied Probability Trust 1999 

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