DocumentCode
1585757
Title
Prototype design and test results of a high temperature remote actuator controller
Author
Shi, Fong ; Martin, Ken
Author_Institution
Boeing Inf. Space & Defense Syst., Seattle, WA, USA
fYear
1998
Firstpage
1
Lastpage
4
Abstract
This report presents an early “Proof-of-Concept” prototype for a distributed aircraft actuator controller operable at 155°C. The prototype employs a minimum number of parts and offers features such as ratiometric position sensing and a pulse width modulated valve drive. Test results are also presented and discussed
Keywords
aircraft control; avionics; distributed control; electric actuators; electrohydraulic control equipment; high-temperature electronics; position measurement; 155 C; distributed aircraft actuator controller; electrohydraulic valve interface circuit; high temperature remote actuator controller; linear variable differential transformers; precision op amps; proof-of-concept prototype; pulse width modulated valve drive; ratiometric position sensing; test results; Actuators; Aerospace control; Aircraft; Distributed control; Prototypes; Pulse width modulation; Space vector pulse width modulation; Temperature sensors; Testing; Valves;
fLanguage
English
Publisher
ieee
Conference_Titel
High Temperature Electronics Conference, 1998. HITEC. 1998 Fourth International
Conference_Location
Albuquerque, NM
Print_ISBN
0-7803-4540-1
Type
conf
DOI
10.1109/HITEC.1998.676750
Filename
676750
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