Our current research projects include nonlinear aeroelasticity and flight dynamics of highly flexible aircraft with integrated multi-functional wings, performance optimization and control of mission adaptive aircraft, and analysis of morphing aircraft with variable compliant wing cambers. Additionally, we have extended our structural dynamics research to the astronautics region, such as the real-time simulation and control of flexible launch vehicles. Click the links below to view the details about the projects.
- Integrated Highly Flexible Multifunctional Wings
- Real-Time Simulation and Control of Flexible Launch Vehicles
- Optimum Performance and Control of Highly Flexible Mission Adaptive Aircraft
- Morphing Aircraft with Compliant Variable Wing Cambers
Previous research topics can be found here: