Effect of actuator nonlinearities on aeroservoelasticity

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 2, 1996, Pages 309-315

  Taylor, Richard ^a,c   Pratt, Roger W ^a,c   Caldwell, Brian D ^b,d  

^a LOUGHBOROUGH UNIVERSITY   (United Kingdom)

^b BAE SYSTEMS   (United Kingdom)

^c Dept Aero Automot Eng Transp S ^*

^d Military Aircraft Division

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT MANUFACTURE; CONTROL NONLINEARITIES; CONTROL SYSTEMS; DYNAMIC RESPONSE; FLIGHT DYNAMICS; MILITARY AIRCRAFT; SERVOMECHANISMS; STRUCTURAL DESIGN;

ACTUATOR NONLINEARITIES; AIRCRAFT STRUCTURE; FLIGHT CONTROL SYSTEM; STRUCTURAL MODE FILTER DESIGN;

AERODYNAMICS;

EID: 0030105517     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21620     Document Type: Article

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