Multi-rotorcraft ground station positioning infrared beacon system
A rotorcraft and ground station technology, applied in the field of measurement, can solve problems such as inability to locate and insufficient positioning accuracy of multi-rotor aircraft
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Embodiment 1
[0049] Multi-rotor ground station positioning infrared beacon system, including: multi-rotor control system, ground station and receiver installed on the multi-rotor;
[0050] The ground station includes: MCU, I / O module, and four infrared arrays; the I / O module and infrared light-emitting diodes are all connected to the MCU for data;
[0051] The infrared array is a sphere, which is closely arranged and then fixed together by a plurality of infrared light-emitting diodes.
[0052] The MCU separately controls the working status and flashing frequency of each infrared array;
[0053] The I / O module is the interface between the MCU and the outside, which is convenient for the user to input the code into the MCU. The MCU uses the "frequency shift keying (FSK)" signal with 38kHZ as the carrier to drive the infrared light-emitting diode according to the specific code.
[0054] The receiver includes: BCM2837, adjustment seat, filter (noise reduction module), infrared camera 1 (Rasp...
Embodiment 2
[0069] Example 2 (eg image 3 shown)
[0070] Compared with Embodiment 1, the only difference is that one of the four infrared arrays is a calibration array, and the direction of the calibration array is defined as the positive direction. When the multi-rotor needs to land: 1. First identify the calibration array from the four infrared arrays. The second processor independently controls the four infrared arrays. The information (flicker frequency) that can be conveyed by the four infrared arrays is different from each other. Therefore, one infrared array can be randomly selected as the positive direction calibration 5, and the remaining infrared arrays 4 are used for other directions. calibration.
[0071] During the landing process, the multi-rotor aircraft first rotates and stops at a certain distance above the ground station, adjusts the beacon sensor to the horizontal downward state and locks it. Then keep the yaw axis YAW axis (that is, the Z axis) still after adjustin...
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