DocumentCode :
670300
Title :
HardWare-In-The-Loop simulation table for UAV navigation complexes testing
Author :
Sineglazov, V.M. ; Dolgorukov, S.O.
Author_Institution :
Aviation Comput.-Integrated Complexes Dept., Nat. Aviation Univ., Kiev, Ukraine
fYear :
2013
fDate :
15-17 Oct. 2013
Firstpage :
141
Lastpage :
145
Abstract :
There are considered peculiarities of multichannel automated control system technical implementation for hardware in the loop simulation table. There were researched ways of decreasing the transmission lines number to provide reliable data acquisition through noisy environment, there was found out that chosen analog to digital converters provide fast, accurate and high resolution data acquisition; implemented data interfaces in FPGA was verified with the computer integrated systems of designing very-large-scale integration digital systems Active-HDL and Quartus II.
Keywords :
aerospace computing; aerospace control; autonomous aerial vehicles; control engineering computing; data acquisition; field programmable gate arrays; Active-HDL; FPGA; Quartus II; UAV navigation complexes testing; analog to digital converter; computer integrated system; data acquisition; hardware-in-the-loop simulation table; multichannel automated control system; transmission lines number; very-large-scale integration digital system; Control systems; Data communication; Hardware; Noise; Propagation delay; Synchronization; Unmanned aerial vehicles; HardWare-In-the-Loop; UAV; navigation complex;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD), 2013 IEEE 2nd International Conference
Conference_Location :
Kiev
Print_ISBN :
978-1-4799-3305-1
Type :
conf
DOI :
10.1109/APUAVD.2013.6705307
Filename :
6705307
Link To Document :
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