Acceleration feedback-based active and passive vibration control of landing gear components

Journal of Aerospace Engineering

Volumn 15, Issue 1, 2002, Pages 1-9

  Kwak, Seung Keon ^a   Washington, Gregory ^b   Yedavalli, Rama K ^b  

^a QRDC Inc   (United States)

^b The Ohio State University   (United States)

Author keywords

Acceleration; Aircraft; Methodology; Vibration control

Indexed keywords

ACCELERATION; ACCELERATION MEASUREMENT; ACTUATORS; COMPUTER SIMULATION; DAMPING; FEEDBACK CONTROL; FINITE ELEMENT METHOD; LANDING GEAR (AIRCRAFT); OPTIMAL CONTROL SYSTEMS; PIEZOELECTRIC DEVICES; STATE SPACE METHODS;

BEAM TYPE DYNAMIC ABSORBER; PIEZOELECTRIC ACTUATORS; RECIPROCAL STATE SPACE METHOD;

VIBRATION CONTROL;

EID: 0036160723     PISSN: 08931321     EISSN: None     Source Type: Journal    
DOI: 10.1061/(ASCE)0893-1321(2002)15:1(1)     Document Type: Article

References (24)

1. Vibration control of beams by beam-type dynamic vibration absorbers
2. Finite element method for piezoelectric vibration
3. Use of active constrained-layer damping for controlling resonant vibration
4. Distributed piezoelectric-polymer active vibration control of a cantilever beam
5. Induced strain actuation of composite beam and rotor blades with embedded piezoceramic elements
6. Smart structure control in matrix second-order form
7. Integrated aeroelastic control optimization of laminated composite lifting surfaces
8. Positive position feedback control for large space structures
9. Some design considerations for active and passive constrained layer damping treatments
10. Effect of tuned dampers on vibrations of simple structure
11. Reduction of steady-state forced vibrations of structures with dynamic absorbers
12. Active and passive vibration control of landing gear components
13. Full state derivative feedback control based on the reciprocal state space framework using smart materials
14. New modeling and control design techniques for smart deformable aircraft structures with acceleration feedback
15. Computational methods in structural dynamics
16. Vibration of cantilever beams to which dynamic absorbers are attached
17. Control design of linear dynamic system with matrix differential equations for equations for aerospace applications
18. Improved aircraft roll maneuver performance using smart deformable wings