An Overview of SensorCraft Capabilities and Key Enabling Technologies
Author:
Affiliation:
1. U.S.. Air Force
2. Air Force Research Laboratory
3. Lockheed Martin Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7185
Reference22 articles.
1. 1D.J.Lucia, "TheSensorCraftCongurations:ANon-LinearAeroServoElasticChallengefor Aviation", AIAA-2005-1943
2. 2C.Tilmann,P.Flick,"HIGHL/DACTIVE(HiLDA)WINGTECHNOLOGIESFOR SENSORCRAFT", AIAA-2003-ICAS
3. Joined-Wing Aeroelastic Design with Geometric Nonlinearity
4. 4E.Reichenbach,"AeroservoelasticDesignandTestValidationoftheJoinedWing Sensorcraft, AIAA-2008-7189
5. 5M.Love,S.Zink,"BodyFreedomFlutterofahighAspectRatioFlyingWing",AIAA-2005-1947
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