Abstract
Based on the dynamical characteristics for UAV with all wheels in ground motion, the whole nonlinear model was established. And the simulation system for the model was designed with the simulation environment of MATLAB/ SIMULINK. Because of including the anti-skid braking system model, it accurately reflects the actual characteristics of the UAV much more. The control system for a flying-wing UAV in ground motion was designed applying drag rudder. And the simulation results of the flying-wing UAV in ground motion during landing indicate that the model can be used, and the UAV control system applying rear wheel braking and drag rudder control corresponded has smooth control response and good performance in ground motion.
| Original language | English |
|---|---|
| Pages (from-to) | 118-122 |
| Number of pages | 5 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 23 |
| Issue number | 1 |
| State | Published - Jan 2011 |
| Externally published | Yes |
Keywords
- Drag rudder
- Flying-wing UAV
- Landing
- Mathematical model
- Simulation