Ground Servoelasticity Test and Analysis of UAVs With Large Aspect Ratio and Joined-Wing Layout
Author:
Affiliation:
1. Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, China
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx8/6287639/10380310/10591964.pdf?arnumber=10591964
Reference20 articles.
1. Aero-structural design of joined-wing aircraft based on high-fidelity model
2. Computational optimal launching control for balloon-borne solar-powered unmanned aerial vehicles in near-space
3. Accelerometer Fault-Tolerant Model-Aided State Estimation for High-Altitude Long Endurance UAV
4. Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future
5. Aeroservoelastic Design and Test Validation of the Joined Wing Sensorcraft
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