A multivariable z-domain linear technique is presented for analyzing a simplified linear HWIL (hardware-in-the-loop) simulation model. Four complementary methods are given, consisting of singular value plots of the input LTF (loop transfer function), multivariable stability margins, closed-loop z-plane poles and zeros of the airframe, and the closed-loop system time response.
Control system analysis of a hardware-in-the-loop simulation
Steuersystemanalyse einer Schleifensimulation
IEEE Transactions on Aerospace and Electronic Systems ; 26 , 4 ; 666-669
1990
4 Seiten, 10 Quellen
Aufsatz (Zeitschrift)
Englisch
MEHRGROESSENREGELUNG , MILITAERISCHES GERAET , UEBERTRAGUNGSFUNKTION , ZEITVERHALTEN , UNENDLICHKEITSSTELLE , NULLSTELLE , ANALYTISCHE FUNKTION , Z-TRANSFORMATION , DIGITALE SIGNALVERARBEITUNG , DIGITALSIMULATION , FLUGKOERPER , STABILITAET , FLUGZEUG , REGELUNGSANALYSE , FLUGZEUGZELLE , POLES AND ZEROS , HARDWARE-IN-THE-LOOP SIMULATION
Hardware in the Loop Simulation of an Attitude Control System
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