1. An aircraft control system, characterized in that the system comprises: the system comprises an aircraft host, a bracelet, an intelligent sound box and an aircraft control server;

the bracelet comprises a first communication module and a first controller which are connected with each other, and a take-off key, a landing key, a switch key, a voice recognition module and a gravity sensing module which are connected with the first controller;

the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module is communicated with the first communication module of the bracelet;

the bracelet is used for sending the voice signal and the gravity sensing signal which are respectively collected by the voice recognition module and the gravity sensing module to the intelligent sound box;

the intelligent sound box is used for decoding and uploading the received voice signal and the gravity sensing signal to the aircraft control server;

the aircraft control server is used for converting the decoded voice and gesture codes into corresponding operation instructions and uploading the operation instructions to the cloud end, so that the cloud end sends the operation instructions to the aircraft host machine to control the flight path and the flight direction of the aircraft.

2. The system of claim 1, wherein the smart sound box is further configured to locate and alert the aircraft host in real time.

3. The system of claim 1, wherein the smart sound box is further configured to automatically return to a take-off point for charging when the charge level of the aircraft host is below a set threshold.

4. The system of claim 1, wherein the bracelet further comprises a power display light, the power display light being connected with the first controller; the bracelet is used for being in according to the real-time electric quantity of aircraft that receives the electric quantity display lamp carries out the electric quantity and shows.

5. The system of claim 1, wherein the aircraft host further comprises a charging module, the charging module coupled to the lithium battery.

6. The system of claim 1, wherein a takeoff key and a landing key of the bracelet are used to control takeoff and landing of the aircraft host.

7. The system of claim 1, wherein the bracelet and the smart speaker are further configured to engage in voice chat interactions.

8. The system of claim 1, wherein the camera in the host aircraft is configured to capture images after the aircraft is started.

9. A method of manufacturing an aircraft, the method comprising:

the bracelet transmits voice signals and gravity sensing signals respectively acquired by the voice recognition module and the gravity sensing module to the intelligent sound box;

the intelligent sound box decodes and uploads the received voice signal and the received gravity sensing signal to an aircraft control server;

the aircraft control server converts the decoded voice and gesture codes into corresponding operation instructions and uploads the operation instructions to the cloud;

and the cloud sends the operating instruction to the aircraft host to control the flight path and the flight direction of the aircraft.

10. The method of claim 9, wherein the bracelet comprises a first communication module and a first controller connected to each other, and a take-off button, a landing button, a switch button, a voice recognition module and a gravity sensing module connected to the first controller;

the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module communicates with the first communication module of the bracelet.

Background

The unmanned aerial vehicle is a comprehensive high-tech product across industries and science. With the development of mechanics, thermodynamics, materials science, artificial intelligence, computer technology, microelectronic technology and communication technology related to aviation development, a batch of brand new military and civil aviation aircrafts with high performance, high efficiency and informatization are born.

The application of the unmanned aerial vehicle is permeating into various industries, and along with the increasing popularization of the civil use of the unmanned aerial vehicle, the requirements of providing stable communication between the unmanned aerial vehicle and the control device of the unmanned aerial vehicle and on the aspects of user experience and air safety become more and more urgent.

Disclosure of Invention

Therefore, the aircraft control system and the aircraft control method are complete in function, the aircraft control tends to be simpler and more intelligent, the structure is relatively simple, the aircraft control system is easy to manufacture, and the aircraft control system and the aircraft control method are suitable for industrial mass production.

In order to achieve the above object, the embodiments of the present application provide the following technical solutions:

according to a first aspect of embodiments of the present application, there is provided an aircraft control system, the system comprising: the system comprises an aircraft host, a bracelet, an intelligent sound box and an aircraft control server;

the bracelet comprises a first communication module and a first controller which are connected with each other, and a take-off key, a landing key, a switch key, a voice recognition module and a gravity sensing module which are connected with the first controller;

the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module is communicated with the first communication module of the bracelet;

the bracelet is used for sending the voice signal and the gravity sensing signal which are respectively collected by the voice recognition module and the gravity sensing module to the intelligent sound box;

the intelligent sound box is used for decoding and uploading the received voice signal and the gravity sensing signal to the aircraft control server;

the aircraft control server is used for converting the decoded voice and gesture codes into corresponding operation instructions and uploading the operation instructions to the cloud end, so that the cloud end sends the operation instructions to the aircraft host machine to control the flight path and the flight direction of the aircraft.

Optionally, the smart sound box is further configured to perform real-time positioning and alarm reminding on the aircraft host.

Optionally, the smart sound box is further configured to automatically return to a departure point for charging when the electric quantity of the aircraft host is lower than a set threshold.

Optionally, the bracelet further comprises an electric quantity display lamp, and the electric quantity display lamp is connected with the first controller; the bracelet is used for being in according to the real-time electric quantity of aircraft that receives the electric quantity display lamp carries out the electric quantity and shows.

Optionally, the aircraft host further comprises a charging module, and the charging module is connected with the lithium battery.

Optionally, the takeoff key and the landing key of the bracelet are used for controlling takeoff and landing of the aircraft.

Optionally, the bracelet and the smart speaker are further configured to perform voice chat interaction.

Optionally, a camera in the aircraft host is used for image acquisition after the aircraft is started.

According to a second aspect of embodiments of the present application, there is provided an aircraft manufacturing method, the method comprising:

the bracelet transmits voice signals and gravity sensing signals respectively acquired by the voice recognition module and the gravity sensing module to the intelligent sound box;

the intelligent sound box decodes and uploads the received voice signal and the received gravity sensing signal to an aircraft control server;

the aircraft control server converts the decoded voice and gesture codes into corresponding operation instructions and uploads the operation instructions to the cloud;

and the cloud sends the operating instruction to the aircraft host to control the flight path and the flight direction of the aircraft.

Optionally, the bracelet comprises a first communication module and a first controller which are connected with each other, and a take-off key, a landing key, a switch key, a voice recognition module and a gravity sensing module which are connected with the first controller;

the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module communicates with the first communication module of the bracelet.

According to a third aspect of embodiments herein, there is provided an aircraft control system, the system comprising: the device comprises a data acquisition device, a processor and a memory; the data acquisition device is used for acquiring data; the memory is to store one or more program instructions; the processor is configured to execute one or more program instructions to perform the method of any of the second aspects.

According to a fourth aspect of embodiments herein, there is provided a computer-readable storage medium having one or more program instructions embodied therein for performing the method of any of the second aspects.

In summary, embodiments of the present application provide an aircraft control system and method, the system including: the system comprises an aircraft host, a bracelet, an intelligent sound box and an aircraft control server; the bracelet comprises a first communication module and a first controller which are connected with each other, and a take-off key, a landing key, a switch key, a voice recognition module and a gravity sensing module which are connected with the first controller; the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module is communicated with the first communication module of the bracelet; the bracelet is used for sending the voice signal and the gravity sensing signal which are respectively collected by the voice recognition module and the gravity sensing module to the intelligent sound box; the intelligent sound box is used for decoding and uploading the received voice signal and the gravity sensing signal to the aircraft control server; the aircraft control server is used for converting the decoded voice and gesture codes into corresponding operation instructions and uploading the operation instructions to the cloud end, so that the cloud end sends the operation instructions to the aircraft host machine to control the flight path and the flight direction of the aircraft. The functions are complete, the control of the aircraft tends to be simpler and more intelligent, the structure is relatively simple, the manufacture is easy, and the method is suitable for industrial batch production.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It should be apparent that the drawings in the following description are merely exemplary, and that other embodiments can be derived from the drawings provided by those of ordinary skill in the art without inventive effort.

The structures, ratios, sizes, and the like shown in the present specification are only used for matching with the contents disclosed in the specification, so that those skilled in the art can understand and read the present invention, and do not limit the conditions for implementing the present invention, so that the present invention has no technical significance, and any structural modifications, changes in the ratio relationship, or adjustments of the sizes, without affecting the functions and purposes of the present invention, should still fall within the scope of the present invention.

FIG. 1 is a block diagram of an aircraft control system provided in an embodiment of the present application;

FIG. 2 is a schematic structural diagram of a portion of an aircraft control system provided in an embodiment of the present application;

FIG. 3 is a schematic illustration of an aircraft host system workflow provided by an embodiment of the present application;

fig. 4a and 4b are schematic views of a bracelet structure provided in an embodiment of the present application;

fig. 5 is a schematic flowchart of an aircraft control method provided in an embodiment of the present application.

Detailed Description

The present invention is described in terms of particular embodiments, other advantages and features of the invention will become apparent to those skilled in the art from the following disclosure, and it is to be understood that the described embodiments are merely exemplary of the invention and that it is not intended to limit the invention to the particular embodiments disclosed. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Fig. 1 illustrates an aircraft control system provided in an embodiment of the present application, where, as shown in fig. 1, the system includes: aircraft host 101, bracelet 102, smart speaker 103, and aircraft control server 104.

The bracelet 102 comprises a first communication module and a first controller which are connected with each other, and a take-off key, a landing key, a switch key, a voice recognition module and a gravity sensing module which are connected with the first controller.

The aircraft host 101 comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module is connected with the first communication module of the bracelet 102.

The bracelet 102 is used for sending the voice signal and the gravity sensing signal which are respectively collected by the voice recognition module and the gravity sensing module to the intelligent sound box 103.

And the intelligent sound box 103 is used for decoding and uploading the received voice signal and the gravity sensing signal to the aircraft control server 104.

The aircraft control server 104 is configured to convert the decoded voice and gesture codes into corresponding operation instructions, and upload the operation instructions to the cloud end 105, so that the cloud end sends the operation instructions to the aircraft host 101 to control the flight path and the flight direction of the aircraft.

In a possible implementation manner, the smart sound box 103 is further used for performing real-time positioning and alarm reminding on the aircraft host 101.

In a possible embodiment, the smart sound box 103 is further configured to automatically return to the flying point for charging when the charge of the aircraft host 101 is lower than a set threshold.

In a possible embodiment, the bracelet 102 further comprises a power display lamp, and the power display lamp is connected with the first controller; the bracelet 102 is used for displaying the electric quantity according to the received real-time electric quantity of the aircraft by the electric quantity display lamp.

In a possible embodiment, the aircraft host 101 further comprises a charging module, which is connected to the lithium battery.

In one possible embodiment, the takeoff button and the landing button of the bracelet 102 are used to control the takeoff and landing of the aircraft main unit 101.

In one possible embodiment, the bracelet 102 and the smart speaker 103 are also used for voice chat interaction.

In one possible embodiment, a camera in the aircraft host 101 is used for image acquisition after the aircraft is started.

Fig. 2 shows a block diagram of an aircraft control system provided in an embodiment of the present application, where the bracelet includes a first communication module and a first controller connected to each other, and a take-off button, a landing button, a switch button, a voice recognition module, and a gravity sensing module connected to the first controller; the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module communicates with the first communication module of the bracelet.

Fig. 3 shows a flow chart of a flight control system provided in an embodiment of the present application, where the aircraft control system includes an aircraft host, an intelligent speaker, a server, and a bracelet, a motor is provided around the aircraft host, and a middle bearing part is composed of a processor, a camera, and a lithium battery. Voice recognition module and gravity response module have been installed to the bracelet the inside, and the bracelet outside is by the electric quantity display lamp with take off the button, descend button, switch button and constitute. The bracelet receives aircraft electric quantity and shows, and speech signal and the gravity-feed tank that will gather through speech recognition module and the gravity-feed tank of in the bracelet are answered the signal input.

The intelligent sound box receives signals and then decodes and uploads the signals to the server in a networked state, then converts voice and gesture codes into corresponding operating instructions and uploads the operating instructions to the cloud, and finally the operating instructions are transmitted to the aircraft host, so that the flight path and the flight direction of the aircraft host are remotely controlled, and functions of accurate positioning, undercurrent recharging, alarm reminding and the like are carried out on the aircraft host in real time. Bracelet and intelligent audio amplifier can also carry out the pronunciation and chat interdynamic. Meanwhile, the camera is installed in the aircraft host, and images can be collected and processed after the aircraft is started.

Fig. 4a and 4b show a schematic structural diagram of a bracelet provided by an embodiment of the application, and the bracelet is provided with a type-C interface, a switch key, an electric quantity display area, a take-off key and a landing key. The control of the aircraft through the hand ring is convenient.

The aircraft control system provided by the embodiment of the application has perfect functions, can be more prone to simplification and intellectualization for controlling the aircraft, has a relatively simple structure, is easy to manufacture, and is suitable for industrial batch production.

In summary, embodiments of the present application provide an aircraft control system, the system includes: the system comprises an aircraft host, a bracelet, an intelligent sound box and an aircraft control server; the bracelet comprises a first communication module and a first controller which are connected with each other, and a take-off key, a landing key, a switch key, a voice recognition module and a gravity sensing module which are connected with the first controller; the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module is communicated with the first communication module of the bracelet; the bracelet is used for sending the voice signal and the gravity sensing signal which are respectively collected by the voice recognition module and the gravity sensing module to the intelligent sound box; the intelligent sound box is used for decoding and uploading the received voice signal and the gravity sensing signal to the aircraft control server; the aircraft control server is used for converting the decoded voice and gesture codes into corresponding operation instructions and uploading the operation instructions to the cloud end, so that the cloud end sends the operation instructions to the aircraft host machine to control the flight path and the flight direction of the aircraft. The functions are complete, the control of the aircraft tends to be simpler and more intelligent, the structure is relatively simple, the manufacture is easy, and the method is suitable for industrial batch production.

Based on the same technical concept, an embodiment of the present application further provides an aircraft manufacturing method, as shown in fig. 5, the method includes:

step 501: the bracelet transmits voice signals and gravity sensing signals respectively acquired by the voice recognition module and the gravity sensing module to the intelligent sound box;

step 502: the intelligent sound box decodes and uploads the received voice signal and the received gravity sensing signal to an aircraft control server;

step 503: the aircraft control server converts the decoded voice and gesture codes into corresponding operation instructions and uploads the operation instructions to the cloud;

step 504: and the cloud sends the operating instruction to the aircraft host to control the flight path and the flight direction of the aircraft.

In one possible implementation, the bracelet comprises a first communication module and a first controller which are connected with each other, and a take-off key, a landing key, a switch key, a voice recognition module and a gravity sensing module which are connected with the first controller; the aircraft host comprises a second communication module and a second controller which are connected with each other, and an aircraft motor, a camera and a lithium battery which are connected with the second controller of the aircraft; the second communication module communicates with the first communication module of the bracelet.

Based on the same technical concept, the embodiment of the present application further provides an aircraft control system, where the system includes: the device comprises a data acquisition device, a processor and a memory; the data acquisition device is used for acquiring data; the memory is to store one or more program instructions; the processor is configured to execute one or more program instructions to perform the method.

Based on the same technical concept, the embodiment of the present application also provides a computer-readable storage medium, wherein the computer-readable storage medium contains one or more program instructions, and the one or more program instructions are used for executing the method.

In the present specification, each embodiment of the method is described in a progressive manner, and the same and similar parts among the embodiments are referred to each other, and each embodiment focuses on the differences from the other embodiments. Reference is made to the description of the method embodiments.

It is noted that while the operations of the methods of the present invention are depicted in the drawings in a particular order, this is not a requirement or suggestion that the operations must be performed in this particular order or that all of the illustrated operations must be performed to achieve desirable results. Additionally or alternatively, certain steps may be omitted, multiple steps combined into one step execution, and/or one step broken down into multiple step executions.

Although the present application provides method steps as in embodiments or flowcharts, additional or fewer steps may be included based on conventional or non-inventive approaches. The order of steps recited in the embodiments is merely one manner of performing the steps in a multitude of orders and does not represent the only order of execution. When an apparatus or client product in practice executes, it may execute sequentially or in parallel (e.g., in a parallel processor or multithreaded processing environment, or even in a distributed data processing environment) according to the embodiments or methods shown in the figures. The terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, the presence of additional identical or equivalent elements in a process, method, article, or apparatus that comprises the recited elements is not excluded.

The units, devices, modules, etc. set forth in the above embodiments may be implemented by a computer chip or an entity, or by a product with certain functions. For convenience of description, the above devices are described as being divided into various modules by functions, and are described separately. Of course, in implementing the present application, the functions of each module may be implemented in one or more software and/or hardware, or a module implementing the same function may be implemented by a combination of a plurality of sub-modules or sub-units, and the like. The above-described embodiments of the apparatus are merely illustrative, and for example, the division of the units is only one logical division, and other divisions may be realized in practice, for example, a plurality of units or components may be combined or integrated into another system, or some features may be omitted, or not executed. In addition, the shown or discussed mutual coupling or direct coupling or communication connection may be an indirect coupling or communication connection through some interfaces, devices or units, and may be in an electrical, mechanical or other form.

Those skilled in the art will also appreciate that, in addition to implementing the controller as pure computer readable program code, the same functionality can be implemented by logically programming method steps such that the controller is in the form of logic gates, switches, application specific integrated circuits, programmable logic controllers, embedded microcontrollers and the like. Such a controller may therefore be considered as a hardware component, and the means included therein for performing the various functions may also be considered as a structure within the hardware component. Or even means for performing the functions may be regarded as being both a software module for performing the method and a structure within a hardware component.

The application may be described in the general context of computer-executable instructions, such as program modules, being executed by a computer. Generally, program modules include routines, programs, objects, components, data structures, classes, etc. that perform particular tasks or implement particular abstract data types. The application may also be practiced in distributed computing environments where tasks are performed by remote processing devices that are linked through a communications network. In a distributed computing environment, program modules may be located in both local and remote computer storage media including memory storage devices.

From the above description of the embodiments, it is clear to those skilled in the art that the present application can be implemented by software plus necessary general hardware platform. Based on such understanding, the technical solutions of the present application may be embodied in the form of a software product, which may be stored in a storage medium, such as a ROM/RAM, a magnetic disk, an optical disk, or the like, and includes several instructions for enabling a computer device (which may be a personal computer, a mobile terminal, a server, or a network device) to execute the method according to the embodiments or some parts of the embodiments of the present application.

The embodiments in the present specification are described in a progressive manner, and the same or similar parts among the embodiments are referred to each other, and each embodiment focuses on the differences from the other embodiments. The application is operational with numerous general purpose or special purpose computing system environments or configurations. For example: personal computers, server computers, hand-held or portable devices, tablet-type devices, multiprocessor systems, microprocessor-based systems, set top boxes, programmable electronic devices, network PCs, minicomputers, mainframe computers, distributed computing environments that include any of the above systems or devices, and the like.

The above-mentioned embodiments are further described in detail for the purpose of illustrating the invention, and it should be understood that the above-mentioned embodiments are only illustrative of the present invention and are not intended to limit the scope of the present invention, and any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the scope of the present invention.