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Vertical landing flight envelope definition



dc.contributor.advisorHaniš Tomáš
dc.contributor.authorJack Charles Hooper
dc.date.accessioned2020-09-04T13:56:41Z
dc.date.available2020-09-04T13:56:41Z
dc.date.issued2020-08-28
dc.identifierKOS-1091261802205
dc.identifier.urihttp://hdl.handle.net/10467/90170
dc.description.abstractThis paper will investigate the development of a landing footprint for a re-entry vehicle. Vehicles can re-enter the atmosphere with a range of orientations, velocities and flight path angles. The central question is whether a vehicle with any combination of these states can be brought to an acceptable landing condition at a particular landing site and with a particular landing speed. To aide in this investigation several models must be implemented, including that of the atmosphere, the vehicles, the Earth, and the aerodynamics. A detailed analysis of the aerodynamic model will be treated, and the equations of motion subject to these aerodynamic laws will then be compared to results from existing atmospheric re-entry software. The principles of optimization will then be employed to generate the footprint of landable states, based on maximum and minimum possible downrange distances, for two vehicle concepts.cze
dc.description.abstractThis paper will investigate the development of a landing footprint for a re-entry vehicle. Vehicles can re-enter the atmosphere with a range of orientations, velocities and flight path angles. The central question is whether a vehicle with any combination of these states can be brought to an acceptable landing condition at a particular landing site and with a particular landing speed. To aide in this investigation several models must be implemented, including that of the atmosphere, the vehicles, the Earth, and the aerodynamics. A detailed analysis of the aerodynamic model will be treated, and the equations of motion subject to these aerodynamic laws will then be compared to results from existing atmospheric re-entry software. The principles of optimization will then be employed to generate the footprint of landable states, based on maximum and minimum possible downrange distances, for two vehicle concepts.eng
dc.publisherČeské vysoké učení technické v Praze. Vypočetní a informační centrum.cze
dc.publisherCzech Technical University in Prague. Computing and Information Centre.eng
dc.rightsA university thesis is a work protected by the Copyright Act. Extracts, copies and transcripts of the thesis are allowed for personal use only and at one?s own expense. The use of thesis should be in compliance with the Copyright Act http://www.mkcr.cz/assets/autorske-pravo/01-3982006.pdf and the citation ethics http://knihovny.cvut.cz/vychova/vskp.htmleng
dc.rightsVysokoškolská závěrečná práce je dílo chráněné autorským zákonem. Je možné pořizovat z něj na své náklady a pro svoji osobní potřebu výpisy, opisy a rozmnoženiny. Jeho využití musí být v souladu s autorským zákonem http://www.mkcr.cz/assets/autorske-pravo/01-3982006.pdf a citační etikou http://knihovny.cvut.cz/vychova/vskp.htmlcze
dc.subjectflight envelopecze
dc.subjectlanding footprintcze
dc.subjecttrajectory optimizationcze
dc.subjectre-entrycze
dc.subjecthypersoniccze
dc.subjectsupersoniccze
dc.subjecthigh angle of attackcze
dc.subjectpseudospectralcze
dc.subjectoptimal control problemcze
dc.subjectFlight envelopeeng
dc.subjecttrajectory optimizationeng
dc.subjectaerodynamicseng
dc.subjectre-entryeng
dc.subjecthypersoniceng
dc.subjectsupersoniceng
dc.subjecthigh angle of attackeng
dc.subjectpseudospectraleng
dc.subjectoptimal control problemeng
dc.subjectlanding footprinteng
dc.titleDefinice letové obálky pro vertikální přistánícze
dc.titleVertical landing flight envelope definitioneng
dc.typediplomová prácecze
dc.typemaster thesiseng
dc.contributor.refereeBeneš Petr
theses.degree.disciplineKybernetika a robotikacze
theses.degree.grantorkatedra řídicí technikycze
theses.degree.programmeKybernetika a robotikacze


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