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

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dc.contributor.authorChai, Runqi
dc.contributor.authorSavvaris, Al
dc.contributor.authorTsourdos, Antonios
dc.contributor.authorChai, Senchun
dc.contributor.authorXia, Yuanqing
dc.date.accessioned2018-02-12T16:47:48Z
dc.date.available2018-02-12T16:47:48Z
dc.date.issued2018-01-25
dc.description.abstractThis 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.identifier.citationRunqi 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, pp1575-1588en_UK
dc.identifier.issn0018-9251
dc.identifier.urihttp://dx.doi.org/10.1109/TAES.2018.2798219
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/12981
dc.language.isoenen_UK
dc.publisherIEEEen_UK
dc.rightsAttribution-NonCommercial 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/
dc.subjectModel Predictive Controlen_UK
dc.subjectspacecraft trajectory trackingen_UK
dc.subjectreceding horizon controlen_UK
dc.subjectoptimal controlen_UK
dc.subjecttwo-nested gradient methoden_UK
dc.titleOptimal tracking guidance for aeroassisted spacecraft reconnaissance mission based on receding horizon controlen_UK
dc.typeArticleen_UK

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