F-22 actuator dynamic stiffness (impedance) testing

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 2, Issue , 2007, Pages 1075-1083

  Layton, David S ^a,b,c   Gaines, Vatanna G ^a,c,d  

^a Lockheed Martin Aeronautical Systems   (Georgia)

^b Flutter and Dynamics   (United States)

^c AIAA   (United States)

^d Loads and Criteria ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DATA REDUCTION; FIGHTER AIRCRAFT; FLIGHT CONTROL SYSTEMS; HYDRAULIC MACHINERY; MATHEMATICAL MODELS; STIFFNESS;

HYDRAULIC ACTUATORS; INSTRUMENTATION DESIGN; TEST DATA ANALYSIS; TEST METHODS;

ACTUATORS;

EID: 34547508875     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-1792     Document Type: Conference Paper

References (2)

1. Staff, "F/A-22 Flutter and Divergence Analysis Report for Block II Aircraft, Volume I - Clean Wing Aircraft," Lockheed Martin Aeronautics Company Report 5PC01339C, December 2005.
2. Encarnacion, "F-22 Actuator Impedance and Frequency Response Tests," Lockheed Martin Aeronautics Company Report 5PD00885, June 1998.