Flight control equipment, system and unmanned aerial vehicle
A flight control and flight control module technology, applied in the field of unmanned aerial vehicles, can solve problems such as weak load capacity, equipment that cannot be installed independently in the cabin, and limited application scenarios of avionics equipment, so as to reduce weight and volume, reduce One-time data packaging and classification to ensure the effect of flight control quality
Pending Publication Date: 2020-07-31
重庆市亿飞智联科技有限公司
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- Application Information
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Problems solved by technology
When the fuselage of the UAV is relatively compact or the load capacity is not strong, it is impossible to install these independent devices in the cabin
Greatly limit the application scenarios of avionics equipment
Method used
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[0078] In order to facilitate the understanding of the present application, the present application will be described more fully below with reference to the relevant drawings. A preferred embodiment of the application is shown in the drawings. However, the present application can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of this application more thorough and comprehensive.
[0079] It should be noted that when an element is considered to be "connected" to another element, it may be directly connected to and integrally integrated with the other element, or there may be an intervening element at the same time.
[0080] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the technical field to which this application belongs. The terms used herein in...
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The invention relates to flight control equipment, a flight control system and an unmanned aerial vehicle. The flight control equipment comprises a flight control module, a differential positioning module and a radio frequency transceiver module, wherein the flight control module at least comprises a control bottom plate and a main control module arranged on the control bottom plate, the control bottom plate is further provided with a first inter-plate interface and a second inter-plate interface, the radio frequency transceiver module is electrically connected with the main control module through the first inter-board interface, the differential positioning module is electrically connected with the main control module through the second inter-board interface, and the radio frequency transceiver module and the differential positioning module are arranged on the upper side and the lower side of the control bottom plate respectively. The flight control equipment is advantaged in that theflight control module, the differential positioning module and the radio frequency transceiving module are integrated together so that the volume of the flight control equipment is reduced by half under the condition of meeting the electrical function, moreover, the weight is greatly reduced, and the working conditions that the unmanned aerial vehicle body is compact and the load-carrying capacity is not high are met.
Description
technical field [0001] The present application relates to the technical field of unmanned aerial vehicles, in particular to a flight control device, system and unmanned aerial vehicles. Background technique [0002] An unmanned aircraft is an autonomous aerial vehicle that can perform multiple missions and can be used multiple times. With the advancement of UAV technology, UAVs have broad application prospects in both military and civil fields. [0003] The current drone avionics are all independent modules, such as independent flight control, independent positioning module, independent radio station, etc. These separate devices are assembled on the drone as separate electronics. When the fuselage of the UAV is relatively compact or the load capacity is not strong, it is impossible to install these independent devices in the cabin. This greatly limits the application scenarios of avionics equipment. Therefore, there is an urgent need for a new type of flight control devi...
Claims
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IPC IPC(8): G05D1/10G05D1/08G01C21/16
CPCG05D1/101G05D1/0816G01C21/165
Inventor 王少平
Owner 重庆市亿飞智联科技有限公司