In this paper,a nonlinear°ight control law is designed for a hybrid unmanned aerial vehicle(UAV)to achieve the advanced°ight performances with the autonomous mission management(AMM).The hybrid UAV is capable...In this paper,a nonlinear°ight control law is designed for a hybrid unmanned aerial vehicle(UAV)to achieve the advanced°ight performances with the autonomous mission management(AMM).The hybrid UAV is capable of hovering like quadrotors and maneuvering as-xed-wing aircraft.The main idea is to design the°ight control laws in modules.Those modules are organized online by the autonomous mission management.Such online organization will improve the UAV autonomy.One of the challenges is to execute the transition°ight between the rotary-wing and-xed-wing modes.The resulting closed-loop system with the designed°ight control law is veri-ed in simulation and the simulation results demonstrate that the resulting closed-loop system can successfully complete the designated°ight missions including the transition°ight between the rotary-wing and-xed-wing modes.展开更多
文摘In this paper,a nonlinear°ight control law is designed for a hybrid unmanned aerial vehicle(UAV)to achieve the advanced°ight performances with the autonomous mission management(AMM).The hybrid UAV is capable of hovering like quadrotors and maneuvering as-xed-wing aircraft.The main idea is to design the°ight control laws in modules.Those modules are organized online by the autonomous mission management.Such online organization will improve the UAV autonomy.One of the challenges is to execute the transition°ight between the rotary-wing and-xed-wing modes.The resulting closed-loop system with the designed°ight control law is veri-ed in simulation and the simulation results demonstrate that the resulting closed-loop system can successfully complete the designated°ight missions including the transition°ight between the rotary-wing and-xed-wing modes.
