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Títol: Design of launcher guidance and control in the frame of avionics architecture


Director/a: BERTRAN ALBERTÍ, EDUARD

Departament: TSC

Títol: Design of launcher guidance and control in the frame of avionics architecture

Data inici oferta: 24-01-2020     Data finalització oferta: 24-09-2020



Estudis d'assignació del projecte:
    DG ENG AERO/SIS TEL
Tipus: Individual
 
Lloc de realització: Fora UPC    
 
        Supervisor/a extern: Eduard Diez Lledó
        Institució/Empresa: GTD
        Titulació del Director/a: Dr. Ciencia y Tecnología Aeroespacial
 
Paraules clau:
guidance, control, launch vehicle, launcher, avionics, spaceflight
 
Descripció del contingut i pla d'activitats:
The goal of this work, integrated in a Horizon 2020 programme developed at GTD, is to design the guidance and control of a small launch vehicle in the first step of an iterative design loop approach. The work focuses on conceiving them not as isolated elements but as parts of a bigger flight software and in the frame of a whole avionics system, converging with its design requirements and constraints. Its final purpose is to produce a restricted frame for future, precise launcher and mission-specific designs.
 
Overview (resum en anglès):
The goal of this work, integrated in a Horizon 2020 programme developed at GTD, is to design the guidance and control of a small launch vehicle in the first step of an iterative design loop approach. The work focuses on conceiving them not as isolated elements but as parts of a bigger flight software and in the frame of a whole avionics system, converging with its design requirements and constraints. Its final purpose is to produce a restricted frame for future, precise launcher and mission-specific designs.


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