Comparison of piezoelectric systems and aerodynamic systems for aircraft vibration alleviation

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 3326, Issue , 1998, Pages 13-26

  Becker, Jürgen ^a   Luber, Wolfgang ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; ELASTICITY; MILITARY AIRCRAFT; PIEZOELECTRICITY; VIBRATIONS (MECHANICAL);

FLIGHT CONTROL SYSTEMS (FCS);

FLIGHT DYNAMICS;

EID: 0032401245     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.310653     Document Type: Conference Paper

References (7)

1. Flutter investigations on a combat aircraft with a command and stability augmentation system
2. Active control of flutter and vibrations of an aircraft
3. Aeroservoelastic stability of aircraft at high incidence
4. Structural aspects of active control technology
5. Unsteady aerodynamic forces at high incidence and their application in structural- and flight control design
6. Aeroservoelastic design, test verification and clearance of an advanced flight control system