A switching control method for a modular variable UAV system
A control method and technology for unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, can solve the problems of insufficient load capacity, short battery life, inability to carry heavy objects, etc., to ensure rapidity and robustness, and to eliminate system chattering Effect
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0097] Such as Figure 1-3 A modular variable unmanned aerial vehicle system is shown, including an unmanned aerial vehicle module and a platform module. The UAV module includes an outer frame and a quadrotor UAV arranged in the outer frame, the outer frame is a regular hexagonal prism frame structure; the quadrotor UAV includes a power supply, flight control, motor, machine arm and propeller, power supply The flight control is placed in the middle quadrilateral cabin cover, the motor is fixed in the arm, and the propeller is a double blade; the outer frame of the UAV module is connected with the arm of the quadrotor UAV, and a tripod is installed at the bottom of the outer frame . The platform module includes an onboard computer, an annular light strip and a docking mechanism. The platform module is a regular hexagonal prism. The onboard computer is placed in a circular cabin cover in the middle, and the annular light strip is arranged around the cabin cover. Changes to displ...
Embodiment 2
[0101] When the UAV module is flying alone, the flight is controlled by its own flight control system. When the connection between the UAV module and the platform module is completed, its control authority is delivered to the onboard computer flight control system on the platform module. And the flight control of the onboard computer and the flight control of a UAV module constitute the master-slave redundant backup flight control system. In this way, when the main flight control fails, the seamless switching of the master-slave flight control can be realized, and the safety of the overall unit can be improved.
[0102] The main-slave redundant backup flight control system includes a main flight control system and a slave flight control system, the main flight control system includes a main flight control controller and a sensor module connected to the main flight control controller; The control system includes a secondary flight control controller and a sensor module connecte...
Embodiment 3
[0111] During the flight of a UAV group composed of multiple UAV modules and platform modules, when a UAV module is low in power, the flight control system of the UAV group sends a call request to the UAV base station on the ground , and send its own location information, the UAV base station calls the UAV module with sufficient power to take off, and performs rough navigation based on GPS to make the UAV module with sufficient power fly to the side of the UAV group and enter the accompanying flight stage , through a method of air docking, replace the UAV module with insufficient power, and the UAV module with insufficient power returns to the UAV base station for charging with the remaining power, waiting for the next call. The UAV base station can be set at a certain distance. When replacing the UAV module, select the nearest base station to call the UAV module.
[0112] When the UAV unit replaces the power supply, the power management system ensures the stability of the vol...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


