Optimal tracking guidance for aeroassisted spacecraft reconnaissance mission based on receding horizon control

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dc.contributor.author Chai, Runqi
dc.contributor.author Savvaris, Al
dc.contributor.author Tsourdos, Antonios
dc.contributor.author Chai, Senchun
dc.contributor.author Xia, Yuanqing
dc.date.accessioned 2018-02-12T16:47:48Z
dc.date.available 2018-02-12T16:47:48Z
dc.date.issued 2018-01-25
dc.identifier.citation Runqi Chai, Al Savvaris, Antonios Tsourdos et. al. Optimal tracking guidance for aeroassisted spacecraft reconnaissance mission based on receding horizon control. IEEE Transactions on Aerospace and Electronic Systems, Volume 54, Issue 4, August 2018, pp1575-1588 en_UK
dc.identifier.issn 0018-9251
dc.identifier.uri http://dx.doi.org/10.1109/TAES.2018.2798219
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/12981
dc.description.abstract This paper focuses on the application of model predictive control (MPC) for the spacecraft trajectory tracking problems. The motivation of the use of MPC, also known as receding horizon control, relies on its ability in dealing with control, state and path constraints that naturally arise in practical trajectory planning problems. Two different MPC schemes are constructed to solve the reconnaissance trajectory tracking problem. Since the MPC solves the online optimal control problems at each sampling instant, the computational cost associated with it can be high. In order to decrease the computational demand due to the optimization process, a newly proposed two-nested gradient method is used and embedded in the two MPC schemes. Simulation results are provided to illustrate the effectiveness and feasibility of the two MPC tracking algorithms combined with the improved optimization technique. en_UK
dc.language.iso en en_UK
dc.publisher IEEE en_UK
dc.rights Attribution-NonCommercial 4.0 International
dc.rights.uri http://creativecommons.org/licenses/by-nc/4.0/
dc.subject Model Predictive Control en_UK
dc.subject spacecraft trajectory tracking en_UK
dc.subject receding horizon control en_UK
dc.subject optimal control en_UK
dc.subject two-nested gradient method en_UK
dc.title Optimal tracking guidance for aeroassisted spacecraft reconnaissance mission based on receding horizon control en_UK
dc.type Article en_UK


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