Higher Level Aerodynamic Input for Aeroservoelastic control of Flexible Aircraft-Reference-Cited by-同舟云学术

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Higher Level Aerodynamic Input for Aeroservoelastic control of Flexible Aircraft

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Mangalam Siva¹,Flick Peter²,Brenner Martin³

Affiliation:

1. Tao of Systems Integration, Inc.

2. Air Force Research Laboratory

3. NASA Dryden Flight Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6380

Reference22 articles.

1. Flow Control Research and Applications at the AFRL's Air Vehicles Directorate

2. The SensorCraft Configurations: A Non-Linear AeroServoElastic Challenge for Aviation

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2. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs;Journal of Aircraft;2018-01

3. Unsteady Aerodynamic Model Based on the Leading-Edge Stagnation Point;Journal of Aircraft;2016-11

4. A Load-Based Feedback Approach for Distributed Aeroservoelastic Control;AIAA Atmospheric Flight Mechanics Conference;2016-06-10

5. An Unsteady Aerodynamic Model based on the Leading-Edge Stagnation Point;33rd AIAA Applied Aerodynamics Conference;2015-06-19

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