Prototyping Framework for Digital Flight Control System
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26230%2F13%3APU106425" target="_blank" >RIV/00216305:26230/13:PU106425 - isvavai.cz</a>
Výsledek na webu
<a href="http://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=6712632" target="_blank" >http://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=6712632</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/DASC.2013.6712632" target="_blank" >10.1109/DASC.2013.6712632</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Prototyping Framework for Digital Flight Control System
Popis výsledku v původním jazyce
Hardware-in-the-loop simulations are indisputably perceived as an integral part of the avionics design and development process. This paper describes a prototyping framework, which has been employed to develop a digital autopilot for a light sport aircraft. Related simulation processes have been performed on two different ground-testing levels. The first level consisted of a laboratory grade development and testing phase, which supported the initial functional estimate of the designed and implemented autopilot features. The subsequent testing level already included the embedded autopilot system installation on board of the test aircraft. System prototyping was performed at the light aircraft simulation lab SimStar at the Brno University of Technology. Additional ground simulations were employed to verify and ground test the operational suitability of the designed autopilot flight control system elements. The implemented hardware units were connected into the simulation network using the CANaerospace communication protocol. Simulations focused on the real time automatic flight modes operational scenarios and confirmed the anticipated performance of the autopilot design features.
Název v anglickém jazyce
Prototyping Framework for Digital Flight Control System
Popis výsledku anglicky
Hardware-in-the-loop simulations are indisputably perceived as an integral part of the avionics design and development process. This paper describes a prototyping framework, which has been employed to develop a digital autopilot for a light sport aircraft. Related simulation processes have been performed on two different ground-testing levels. The first level consisted of a laboratory grade development and testing phase, which supported the initial functional estimate of the designed and implemented autopilot features. The subsequent testing level already included the embedded autopilot system installation on board of the test aircraft. System prototyping was performed at the light aircraft simulation lab SimStar at the Brno University of Technology. Additional ground simulations were employed to verify and ground test the operational suitability of the designed autopilot flight control system elements. The implemented hardware units were connected into the simulation network using the CANaerospace communication protocol. Simulations focused on the real time automatic flight modes operational scenarios and confirmed the anticipated performance of the autopilot design features.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
—
OECD FORD obor
10201 - Computer sciences, information science, bioinformathics (hardware development to be 2.2, social aspect to be 5.8)
Návaznosti výsledku
Projekt
<a href="/cs/project/TA01010678" target="_blank" >TA01010678: Chytrý autopilot</a><br>
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Ostatní
Rok uplatnění
2013
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
Proceedings of 32nd Digital Avionics Systems Conference
ISBN
978-1-4799-1536-1
ISSN
—
e-ISSN
—
Počet stran výsledku
12
Strana od-do
1-12
Název nakladatele
IEEE Computer Society
Místo vydání
Syracuse, NY
Místo konání akce
Syracuse, NY
Datum konání akce
6. 10. 2013
Typ akce podle státní příslušnosti
WRD - Celosvětová akce
Kód UT WoS článku
—