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Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/88023
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dc.contributor.authorPrime, Z.-
dc.contributor.authorDoolan, C.-
dc.contributor.authorCazzolato, B.-
dc.contributor.authorBrooks, L.-
dc.date.issued2012-
dc.identifier.citation50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2012, pp.1-12-
dc.identifier.isbn9781600869365-
dc.identifier.urihttp://hdl.handle.net/2440/88023-
dc.description.abstractScramSpace I is a free-flying hypersonic flight vehicle due to be launched in October 2012. The flight dynamics of ScramSpace I are calculated using Newtonian-flow aerody- namics and longitudinal point-mass equations of motion. These flight dynamics are then represented in Linear Parameter Varying (LPV) form using a curve-fit approximation to the true equations of motion. An LPV controller designed using an LQR-like H2 minimi- sation problem problem is designed to stabilise the vehicle during re-entry, and simulation results against the original equations of motion during re-entry are presented.-
dc.description.statementofresponsibilityZebb Prime, Con Doolan, Ben Cazzolato, Laura Brooks-
dc.language.isoen-
dc.publisherAmerican Institute of Aeronautics and Astronautics-
dc.rightsCopyright © 2012 by Zebb Prime-
dc.source.urihttp://dx.doi.org/10.2514/6.2012-255-
dc.titleLongitudinal flight dynamics modelling and control of ScramSpace I-
dc.typeConference paper-
dc.contributor.conference50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (9 Jan 2012 - 12 Jan 2012 : Nashville, Tennessee)-
dc.identifier.doi10.2514/6.2012-255-
pubs.publication-statusPublished-
dc.identifier.orcidCazzolato, B. [0000-0003-2308-799X]-
Appears in Collections:Aurora harvest 7
Mechanical Engineering conference papers

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