Tesi etd-01252019-171312 |
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Tipo di tesi
Tesi di laurea magistrale
Autore
CASCIOLA, LUCA
URN
etd-01252019-171312
Titolo
Control Allocation for a Fully Controllable Aircraft
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Quarta, Alessandro A.
correlatore Prof. Cipolla, Vittorio
correlatore Prof. Cipolla, Vittorio
Parole chiave
- allocazione dei controlli
- CA
- control allocation
- direct lift control
- DLC
- INCA
- inversion
- inversione
- Parsifal
- prandtl
- prandtl-plane
Data inizio appello
19/02/2019
Consultabilità
Completa
Riassunto
Parsifal is a box-wing aircraft with redundant control surfaces that is expected to save fuel during cruise and, making use of the Direct Lift Control, it can perform maneuveurs that other aircraft can't, such as the vertical slide.
The aircraft needed a reliable control system to substitute to the pre-existing PID controls and for this reason Incremental Control Allocation was introduced.
The thesis is focused on the development and test of different versions of such algorithm. The implementation in the aircraft Parsifal showed optimal results in aircraft stability and control.
It follows an extensive description of the software implemented (in Matlab and Simulnk) and an installation guide of the controller block inside any aircraft dynamic system.
The aircraft needed a reliable control system to substitute to the pre-existing PID controls and for this reason Incremental Control Allocation was introduced.
The thesis is focused on the development and test of different versions of such algorithm. The implementation in the aircraft Parsifal showed optimal results in aircraft stability and control.
It follows an extensive description of the software implemented (in Matlab and Simulnk) and an installation guide of the controller block inside any aircraft dynamic system.
File
| Nome file | Dimensione |
|---|---|
| thesis_print.pdf | 13.50 Mb |
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