This paper focuses on the modeling, control, and simulation of an over-actuated htr. This configuration implies that two of the six actuators are independently tilted using servomotors, which provide high maneuverability and reliability. This approach is predicted to maintain zero pitch throughout the trajectory and is expected to improve the aircraft’s steering accuracy. This arrangement is particularly beneficial for pa applications where accurate monitoring and management of crops are critical. The enhanced maneuverability allows for precise navigation in complex vineyard environments, enabling the uav to perform tasks such as aerial imaging and crop health monitoring. The employed control architecture consists of cascaded p-pid controllers using the slc method on the five controlled dof. Simulated results using Gazebo demonstrate that the htr achieves stability and maneuverability throughout the flight path, significantly improving precision agriculture practices. Furthermore, a comparison of the htr with a traditional hexacopter validates the proposed approach.
Read full abstract