Development of DDV (direct drive valve) servo actuator

Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

Volumn 24, Issue 3, 2006, Pages 308-312

  Xia, Liqun ^a   Zhang, Xinguo ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Direct drive valve; Rapid prototyping; Servo actuator

Indexed keywords

AIRCRAFT; FAILURE (MECHANICAL); HYDRAULICS; MONITORING; RAPID PROTOTYPING; REAL TIME SYSTEMS; RELIABILITY; REQUIREMENTS ENGINEERING; VALVES (MECHANICAL);

DIRECT DRIVE VALVE; ELECTRO HYDRAULIC VALVE; SERVO ACTUATOR; SOFTWARE MATLAB;

ACTUATORS;

EID: 33748466943     PISSN: 10002758     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (4)

1. Hsu Y N, Lai C Y, Lee Y K. Development of the Direct Drive Valve (DDV) Actuation System on the IDF Aircraft. International Pacific Air and Space Technology Conference and 29th Aircraft Symposium, Japan, 1991
2. Lin J S, Chen C L, Lai C Y. A High-Bandwidth PWM Servo Amplifier for the Direct-Drive-Valve Actuation System. IEEE Proc Applied Power Electronics Conference and Exposition, 1993, 78: 328-332
3. Vieten K W, Snyder J D, Clark R P. Redundancy Management Concepts for Advanced Actuation Systems. AIAA, Aerospace Design Conference, Irvine, CA, 1993