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24 results on '"Xiang, Jinwu"'

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1. Robot Pilot: A New Autonomous System toward Flying Manned Aerial Vehicles

2. Design and experimental study of a new flapping wing rotor micro aerial vehicle

3. Aerodynamic characteristics of morphing wing with flexible leading-edge

4. Adaptive terminal sliding combined super twisting control design and flight tests for automatic carrier landing system

5. Delaying stall of morphing wing by periodic trailing-edge deflection

6. Design optimization and testing of a morphing leading-edge with a variable-thickness compliant skin and a closed-chain mechanism

7. Numerical simulation of aircraft arresting process with an efficient full-scale rigid-flexible coupling dynamic model

8. Reduced-order modeling of unsteady aerodynamics of a flapping wing based on the Volterra theory.

9. A model updating method considering the complex mechanical environment.

10. Design, Modeling and Analysis of a Sharp-edge Hypersonic Stealthy Re-entry Vehicle.

11. Crashworthiness of Civil Aircraft Subject to Soft Soil and Concrete Impact surface.

12. Static aeroelasticity of the propulsion system of ion propulsion unmanned aerial vehicles

13. Flight safety measurements of UAVs in congested airspace

14. A modified airfoil-based piezoaeroelastic energy harvester with double plunge degrees of freedom

15. Aerodynamic performance of the locust wing in gliding mode at low Reynolds number

16. Crashworthiness analysis of aircraft fuselage with sine-wave beam structure

17. Aerodynamic Performance of the Locust Wing in Gliding Mode at Low Reynolds Number

18. Experimental Validation of an Effective Control Mechanism to Enable Flapping Wing Rotor Stable Flight

19. Modeling of Unsteady Aerodynamics for a Flapping wing

20. A novel trajectory planning strategy for aircraft emergency landing using Gauss pseudospectral method

21. Crashworthiness uncertainty analysis of typical civil aircraft based on Box–Behnken method

22. Modeling and nonlinear aeroelastic analysis of a wing with morphing trailing edge

23. Multi-objective robust airfoil optimization based on non-uniform rational B-spline (NURBS) representation

24. Efficiency evaluation of energy harvesting from discrete gust response for plate wing

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