Actuator Saturation and its Influence on Vibration Reduction by Actively Controlled Flaps

Actuator Saturation and its Influence on Vibration Reduction by Actively Controlled Flaps

Author(s):

Publication title:

A collection of technical papers : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit : AIAA/ASME/ASCE/AHS Adaptive Structures Forum : AIAA Non-Deterministic Approaches Forum : AIAA Gossamer Spacecraft Forum, Seattle, Washington, 16-19 April 2001

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

2001

Pub. Year:

2001

Vol.:

v. 3

No.:

2001-1467

Paper no.:

AIAA-2001-1467

Page(from):

2101

Page(to):

2111

Pages:

11

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563474774 [1563474778]

Language:

English

Call no.:

A07400/011180

Type:

Technical Paper

Details

TDL ID:	ZA00000081
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit ; AIAA/ASME/ASCE/AHS Adaptive Structures Forum ; AIAA Non-Deterministic Approaches Forum ; AIAA Gossamer Spacecraft Forum
Conf. info. (Venue):	Seattle, Washington
Conf. info. (Date):	2001.04.16-2001.04.19

Similar Items:

1 Technical Paper Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap Friedmann, P., Depailler, G. American Institute of Aeronautics and Astronautics	7 Technical Paper Vibration Reduction and Performance Enhancement of Helicopter Rotors Using an Active/Passive Approach B. Glaz, P. Friedmann, L. Liu American Institute of Aeronautics and Astronautics
2 Technical Paper Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade Millott, T. A., Friedmann, P. P. National Aeronautics and Space Adminstration	8 Technical Paper Experimental Studies on Different Actuator-Sensor Configurations of Active Control Systems for the Reduction of Noise and Vibration in Vehicles J. Millitzer, D. Mayer, R. Kraus, M. Schmidt Society of Automotive Engineers
3 Technical Paper Helicopter Noise Reduction By Actively Controlled Flaps Patt, D., Liu, L., Friedmann, P. American Institute of Aeronautics and Astronautics	9 Technical Paper Application of a Weighted Average Surrogate Approach to Helicopter Rotor Blade Vibration Reduction B. Glaz, T. Goel, L. Liu, P. Friedmann, R. Haftka American Institute of Aeronautics and Astronautics
4 Technical Paper Vibration Reduction and Performance Enhancement in Rotorcraft Using Active Flaps at High Advance Ratios L. Liu, P. Friedmann, I. Kim, D. Bernstein American Institute of Aeronautics and Astronautics	10 Technical Paper Rotary-wing aeroelastic scaling and its application to adaptive materials based actuation Friedmann, Peretz P. American Institute of Aeronautics and Astronautics
5 Technical Paper Unsteady compressible aerodynamics of a flapped airfoil with application to helicopter vibration reduction Myrtle, Timothy F., Friedmann, Peretz P. American Institute of Aeronautics and Astronautics	11 Technical Paper Optimal Placement of Piezoelectric Actuated Trailing-Edge Flaps for Helicopter Vibration Control S. Viswamurthy, R. Ganguli American Institute of Aeronautics and Astronautics
6 Technical Paper Vibration suppression in helicopters using the ACSR approach with improved aerodynamic modeling Cribbs, Richard C., Friedmann, Peretz P. American Institute of Aeronautics and Astronautics	12 Technical Paper Active Flow Control for High Lift Airfoils: Dynamic Flap Actuation J. Kiedaisch, B. Demanett, P. Reinhard, H. Nagib American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12