Dynamic loading systems for ground testing of high speed aerospace actuators

Aircraft Engineering and Aerospace Technology

Volumn 78, Issue 4, 2006, Pages 275-282

  Mare, Jean Charles ^a  

^a University of Toulouse Clement Ader Institute   (France)

Author keywords

Actuators; Dynamics; Force; Simulation; Tests and testing

Indexed keywords

AEROSPACE APPLICATIONS; AEROSPACE ENGINEERING; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DYNAMICS; TESTING;

CONTROL DESIGN; CONTROLLER ARCHITECTURE; DYNAMIC LOADING SYSTEM; GROUND TESTING;

ACTUATORS;

EID: 33748333383     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/17488840610675546     Document Type: Article

References (5)

1. Bohr, G. and Hamilton, S. (2000), “Force control is the issue in aerospace structural test lab”, Hydraulics and Pneumatics, pp. 43-7.
2. Maré, J-C. (2000a), “Force control of electrohydraulic actuators driving various load mechanical impedances”, Proceedings of the Second Internationales Fluidtechnisches Kolloquium in Dresden, pp. 149-62.
3. Maré, J-C. (2000b), “Considérations pratiques sur les correcteurs PID dans le domaine de l'énergie fluide”, Revue Fluides, Numéro Spécial Matériels, pp. 8-17.
4. Maré, J-C. (2002), “Actionneurs hydrauliques”, Encyclopédie des Techniques de l'Ingénieur, Articles S7530 and 57531, série Mesure et Régulation, p. 35.
5. Maré, J-C. and Cregut, S. (2001), “Electrohydraulic force generator for the certification of a thrust vector actuator”, Proceedings of the International Conference on Recent Advances in Aerospace Actuation Systems and Components, Toulouse, pp. 59-63.