Noniterative System Identification Applied to Wind Tunnel Valve Control

Noniterative System Identification Applied to Wind Tunnel Valve Control

A noniterative system identification procedure is developed and applied to the air supply control valves of a wind tunnel. These control valves regulate the air flow through the wind tunnel and thereby determine the flight conditions being simulated. The position control system for these valves must...

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Veröffentlicht in:IEEE transactions on industrial electronics (1982) 1985-02, Vol.IE-32 (1), p.71-77
Hauptverfasser: Beale, Guy O., Cook, Gerald
Format: Artikel
Sprache:eng
Schlagworte:
Aerospace simulation
Continuous time systems
Control systems
Damping
Frequency
Position control
System identification
System testing
Transfer functions
Valves
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Beschreibung
Zusammenfassung:A noniterative system identification procedure is developed and applied to the air supply control valves of a wind tunnel. These control valves regulate the air flow through the wind tunnel and thereby determine the flight conditions being simulated. The position control system for these valves must be of high performance and should be maintained in a properly tuned condition.
ISSN:0278-0046
1557-9948
DOI:10.1109/TIE.1985.350144