Management platform and method for take-off and landing of rotor unmanned aerial vehicle

A technology of unmanned rotor and management platform, applied in the field of drones, can solve the problems of inability to efficiently utilize the flexibility characteristics of unmanned vehicles and high-load drones, and the degree of automation is not high, so as to achieve efficient search and rescue tasks and improve flexibility Degree, good security effect

Active Publication Date: 2020-09-11
航大汉来(天津)航空技术有限公司
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AI Technical Summary

Problems solved by technology

However, at present, there is still relatively little research on the entire system of drones and unmanned vehicles cooperating to complete the dynamic landing of unmanned vehicles on unmanned vehicles. The characteristics of flexibility still require manual operation to complete the take-off and landing process, and the degree of automation is not high

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  • Management platform and method for take-off and landing of rotor unmanned aerial vehicle
  • Management platform and method for take-off and landing of rotor unmanned aerial vehicle
  • Management platform and method for take-off and landing of rotor unmanned aerial vehicle

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Embodiment

[0039] Example: see Figure 1-5 The invention provides a management platform for take-off and landing of a rotary-wing unmanned aerial vehicle, including a drone flight control device and a control system running on the device.

[0040] The control system includes a flight control module, a visual calculation module and an image acquisition and transmission module, and the flight control module includes a flight control processor and a measurement system, wherein the flight control processor is connected with the visual calculation module for calculating the current attitude and position of the aircraft; The measurement system includes radio altimeter 1, radio altimeter 2, laser inertial navigation / GPS integrated navigation system, main air data computer, backup air data computer, fiber-optic inertial navigation / GPS integrated navigation system, MEMS inertial navigation / GPS integrated navigation system, Dual-antenna differential GPS, main / standby radio link, visual navigation ...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, and particularly relates to a management platform and method for taking off and landing of a rotor unmanned aerial vehicle. The flight control system comprises a flight control device of the unmanned aerial vehicle and a control system running on the device, the unmanned aerial vehicle flight control device is jointly composed of an aircraft and a take-off and landing platform, the aircraft comprises a central fuselage, two main force arms, a longitudinal rotor rod and an undercarriage, and the two main force arms are fixed to the two sides of the central fuselage correspondingly and obliquely arranged upwards; the two longitudinal rotor rods are in one-to-one correspondence with the main force arms; unmanned dynamictake-off and landing are completed through cooperation of the flight control module, the visual calculation module and the image acquisition and transmission module, the unmanned flexibility is greatly improved, and search and rescue tasks can be executed more efficiently.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a management platform and method for take-off and landing of rotary-wing unmanned aerial vehicles. Background technique [0002] Today, UAVs can perform repetitive tasks with high precision. They can be deployed in harsh workplaces with sensors that exceed human perception. UAVs are also used in patrol and search and rescue missions. In the existing technology, we can find examples of the application of unmanned vehicles and unmanned aerial vehicles, but the application scenarios of these two kinds of robots have certain limitations; although the unmanned aerial vehicle has the characteristics of simple operation and flexible flight, However, it is often limited by their limited flight time and relatively low load capacity; while unmanned ground vehicles can operate for a long time and carry a large load, but are limited by limited terrain passing capabilities, s...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D47/08B64F1/00B64F1/02G05D1/06G05D1/10
CPCB64C39/02B64D47/08B64F1/00B64F1/025G05D1/0676G05D1/101
Inventor 黄彦高桓胡亮胡媛彦
Owner 航大汉来(天津)航空技术有限公司
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