Hardware in the Loop Simulation of FBW components
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F09%3A00157936" target="_blank" >RIV/68407700:21220/09:00157936 - isvavai.cz</a>
Alternative codes found
RIV/68407700:21230/09:00157936
Result on the web
—
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Hardware in the Loop Simulation of FBW components
Original language description
The paper presents hardware in the loop simulator developed for validation of control algorithms and electro-hydraulic servo actuators designed for flight by wire control system of a small jet plane. The architecture and functionality of the flight by wire system is briefly described and requirements on validation tests to carry out on the hardware in the loop simulator are mentioned. The flight by wire control system under development consist of dual channel flight control computer and dual channel electronic control unite controlling dual channel electro hydraulic servo actuator with mechanical redundancy. It support several control modes as autopilot and recovery mode. An architecture and software and hardware components of the developed simulator and hydraulic stand are described. The simulator instrumentation is based on distributed peripherals communicating via CANopen industrial field bus.
Czech name
—
Czech description
—
Classification
Type
O - Miscellaneous
CEP classification
JC - Computer hardware and software
OECD FORD branch
—
Result continuities
Project
<a href="/en/project/FT-TA3%2F044" target="_blank" >FT-TA3/044: *Module solution of FLY-BY-WIRE control system for light, jet aircraft.</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2009
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů