Takeoff and landing control device for rotor unmanned aerial vehicle and control method thereof

A technology of unmanned rotor and control device, which is applied in the directions of unmanned aerial vehicle, launch/drag transmission device, motor vehicle, etc., can solve the problem of high terrain requirements, and achieve low terrain correlation, convenient landing and simple structure. Effect

Active Publication Date: 2018-01-19
许金兰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, existing UAVs have high requirements for terrain when taking off and landing, and those skilled i

Method used

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  • Takeoff and landing control device for rotor unmanned aerial vehicle and control method thereof
  • Takeoff and landing control device for rotor unmanned aerial vehicle and control method thereof
  • Takeoff and landing control device for rotor unmanned aerial vehicle and control method thereof

Examples

Experimental program
Comparison scheme
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Example Embodiment

[0024] Example 1

[0025] Such as figure 1 As shown, a take-off and landing control device for a rotary-wing drone includes a base 1 and a floating board take-off platform 2. The base 1 is provided with a storage tank (not shown), the base 1 and the floating board take-off platform 2 A rubber connecting piece 3 is arranged between the base 1 and the floating board take-off platform 2 and the rubber connecting piece 3 is bonded, and the floating board take-off platform 2 and the rubber connecting piece 3 are arranged to cover the slot of the storage tank, The storage tank is filled with liquid metal 4, the storage tank is provided with an electric heating iron 5 and a semiconductor refrigeration sheet 6, and the side of the base 1 is provided with a PLC 8, a battery box 9 and a landing board 10. The landing board 10 is provided with a detection device 11 and an ejection mechanism 12, an electric wire take-up 13 is arranged under the landing plate 10, a wire routing hole 7 is arran...

Example Embodiment

[0027] Example 2

[0028] Such as Figure 1-4 As shown, a take-off and landing control device for a rotary-wing drone includes a base 1 and a floating board take-off platform 2. The base 1 is provided with a storage tank (not shown), the base 1 and the floating board take-off platform 2 A rubber connecting piece 3 is arranged between the base 1 and the floating board take-off platform 2 and the rubber connecting piece 3 is bonded, and the floating board take-off platform 2 and the rubber connecting piece 3 are arranged to cover the slot of the storage tank, The storage tank is filled with liquid metal 4, the storage tank is provided with an electric heating iron 5 and a semiconductor refrigeration sheet 6, and the side of the base 1 is provided with a PLC 8, a battery box 9 and a landing board 10. The landing board 10 is provided with a detection device 11 and an ejection mechanism 12, an electric wire take-up 13 is arranged under the landing plate 10, a wire routing hole 7 is a...

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Abstract

The invention discloses a takeoff and landing control device for a rotor unmanned aerial vehicle (UAV) and a control method thereof. The takeoff and landing control device for the rotor UAV comprisesa base and a floating takeoff platform, wherein the base is provided with a storage tank; rubber connecting pieces are arranged between the base and the floating takeoff platform; both of the base andthe floating takeoff platform are fixedly connected with the rubber connecting pieces; the floating takeoff platform and the rubber connecting pieces cover a tank opening of the storage tank; the storage tank is filled with liquid metal; electric heating iron and a semiconductor cooling piece are arranged inside the storage tank; a PLC, a battery box and a landing board are arranged at the side surface of the base; a detection device and a catapult mechanism are arranged on the landing board; an electric wire-take-up device is arranged below the landing board; and a wire through hole is arranged in the middle of the landing board. The takeoff and landing control device for the rotor UAV allows the UAV to take off and land in a variety of landforms.

Description

technical field [0001] The invention relates to a take-off and landing control device for a rotary-wing unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with a parachute or a block. Can be used ...

Claims

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Application Information

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IPC IPC(8): B64F1/04B64F1/06
CPCB64F1/04B64F1/06B64U70/00
Inventor 李馨嫔王健
Owner 许金兰
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