Glossario (Strumentazione di bordo e avionica)
In questa pagina sono raccolte tutte le parole specifiche, e in particolare gli acronimi, utilizzate durante il corso.
| Indice A B C D E F G H I J K L M N O P Q R S T U V W X Y Z ? |
A
[modifica]AFCS
[modifica]- Automatic Flight Control System: tutti i sistemi che controllano il volo automatico (autopilota, ecc.)
ATP
[modifica]- Acceptance Test Procedure: la procedura per la validazione di un componente al fine di assegnargli la red label.
ARINC
[modifica]- Aeronautical Radio Incorporated
AOI
[modifica]- Automatic Optical Inspection
API
[modifica]- Application Programming Interface
ATE
[modifica]- Automatic Test Equipment
AWG
[modifica]- American Wire Gauge
B
[modifica]BIT
[modifica]- Built-In Test
BITE
[modifica]- Built-In Test Equipment
BPUM
[modifica]- Basic Power Up Manager
BTS
[modifica]- Burn In Test Set
BTP
[modifica]- Burn In Test Procedure
BAFO
[modifica]- Best and Final Offer
BGA
[modifica]- Ball Grid Array
BO
[modifica]- Breakout
BOM
[modifica]- Bill of Material
BU
[modifica]- Business Unit
C
[modifica]C3
[modifica]- Command, Control and Communication
C4I
[modifica]- Command, Control, Communications, Computers, and Intelligence (Vedi la voce relativa su Wikipedia (EN) )
COTS
[modifica]CDR
[modifica]- Critical Design Review
CPLD
[modifica]- Complex Programmable Logic Device
CSCI
[modifica]- Computer Software Configuration Item
CRC
[modifica]- Cyclic Redundancy Check
CoC
[modifica]- Certificate of Conformity
D
[modifica]DDP
[modifica]- Declaration of Design and Performance
DOORS
[modifica]- (software) Dynamic Object Oriented Requirement System
E
[modifica]EASA
[modifica]- European Aviation Safety Agency
EFA
[modifica]- Experimental Flight Approval
EGPWS
[modifica]- Enhanced Ground Proximity Warning System
EMP
[modifica]- ElectroMagnetic Pulse
EVMS
[modifica]- Earned Value Management System
EWS
[modifica]- Engineering Work Statement
F
[modifica]FRACAS
[modifica]- Failure Reporting, Analysis and Corrective Action System
FMECA
[modifica]- Failure Modes, Effects, and Criticality Analysis
FDR
[modifica]- Final Design Review
G
[modifica]H
[modifica]HUMS
[modifica]Healt and Usage Monitoring System
I
[modifica]ICD
[modifica]- Interface Control Document
ILS (1)
[modifica]- Integrated Logistic Support
ILS (2)
[modifica]- Instrumental Landing System
J
[modifica]K
[modifica]L
[modifica]LRU
[modifica]- Line Replacement Unit
M
[modifica]MEL
[modifica]- Minimum Equipment List
MEP
[modifica]- Mission Equipment Package
MTTF
[modifica]- Mean Time To Failure
MTBF
[modifica]- Mean Time Between Failure
MTBMA
[modifica]- Mean Time Between Maintance Action
MTTR
[modifica]- Mean Time To Repair
MTSM
[modifica]- Mean Time for Scheduled Maintenance
MTLA
[modifica]- Mean Time for Logistic Action
N
[modifica]NVG
[modifica]- Night Vision Goggles
O
[modifica]P
[modifica]PDR
[modifica]- Preliminary Design Review
Q
[modifica]QA
[modifica]- Quality Assurance
QC
[modifica]- Quality Control
QM
[modifica]- Quality Management
R
[modifica]RAM
[modifica]- (ufficio) Reliability and Maintenance
S
[modifica]S&R
[modifica]- Search and Rescue
SDD
[modifica]- System Design Document
SRD
[modifica]- System Requirement Document
SRR
[modifica]- System Requirement Review
SRI
[modifica]- Shop Replacement Item
STTE
[modifica]- Special Type Test Equipment
T
[modifica]TCO
[modifica]- Total Cost of Ownership
TSO
[modifica]- Technical Standard Order
TRR
[modifica]- Test Readiness Review
U
[modifica]V
[modifica]V&V
[modifica]- Validation and Verify