Hardware in the Loop Simulation of FBW components

Kód výsledku v 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>

Nalezeny alternativní kódy

RIV/68407700:21230/09:00157936

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Hardware in the Loop Simulation of FBW components

Popis výsledku v původním jazyce

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.

Název v anglickém jazyce

Hardware in the Loop Simulation of FBW components

Popis výsledku anglicky

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.

Druh

O - Ostatní výsledky

CEP obor

JC - Počítačový hardware a software

OECD FORD obor

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Projekt

<a href="/cs/project/FT-TA3%2F044" target="_blank" >FT-TA3/044: *Modulové řešení systému řízení FLY-BY-WIRE pro lehký proudový letoun.</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2009

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů