Integration of a generic flight control system into ASTROS

Author:

Volk J.1,Ausman J.1

Affiliation:

1. Northrop Grumman Corp., Pico Rivera, CA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. An Analysis of the Integration of Active Aeroelastic Wing Technology into a Co-Planar Variable Geometry Morphing Wing;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

2. Maneuver Load Analysis of Overdetermined Trim Systems;Journal of Aircraft;2008-01

3. Integrated Aeroservoelastic Design Optimization of Actively-Controlled Strain-Actuated Flight Vehicles;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18

4. Application of Active-Aeroelastic-Wing Technology to a Joined-Wing Sensorcraft;Journal of Aircraft;2004-05

5. Robust Structural Design of an Active Aeroelastic Wing with Maneuver Load Inaccuracies;Journal of Aircraft;2004-05

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