CN115933501A - Operation control method, device and equipment of rocket control software - Google Patents

Operation control method, device and equipment of rocket control software Download PDF

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Publication number
CN115933501A
CN115933501A CN202310010254.0A CN202310010254A CN115933501A CN 115933501 A CN115933501 A CN 115933501A CN 202310010254 A CN202310010254 A CN 202310010254A CN 115933501 A CN115933501 A CN 115933501A
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China
Prior art keywords
voice
instruction
rocket
control
control software
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CN202310010254.0A
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Chinese (zh)
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文天乐
彭昊旻
布向伟
赵也倪
陈乐�
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Dongfang Space Technology Shandong Co Ltd
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Dongfang Space Technology Shandong Co Ltd
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Priority to CN202310010254.0A priority Critical patent/CN115933501A/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P90/00Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
    • Y02P90/02Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]

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Abstract

The invention provides an operation control method, device and equipment of rocket control software, and relates to the technical field of computer information processing. The method comprises the following steps: acquiring a voice control instruction input through voice input equipment; analyzing the voice control instruction to obtain a voice characteristic signal corresponding to the voice control instruction; if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction; and carrying out operation control on the rocket control software according to the operation. The scheme of the invention realizes the remote control of the rocket control software, so that the operation of the rocket control software is more convenient and faster, and the use threshold of the rocket control software is reduced.

Description

Operation control method, device and equipment of rocket control software
Technical Field
The invention relates to the technical field of computer information processing, in particular to an operation control method, device and equipment of rocket control software.
Background
In a traditional rocket control system, software is required to be manually operated to control the software, operation is required to be performed in a manual clicking mode, and login of a user, control of a process, display of an interface and display of a current running state are achieved by clicking a button.
In the prior art, a user needs to operate software beside a computer to realize rocket control, so that remote control cannot be realized, and meanwhile, in the operation process, an operator needs to know how to operate the software and the positions corresponding to flow keys, so that the operation process is complicated, and the situation of operation errors can occur.
Disclosure of Invention
The invention provides an operation control method, device and equipment of rocket control software. The remote control of the rocket control software is realized, so that the operation of the rocket control software is more convenient and faster, and the use threshold of the rocket control software is reduced.
In order to solve the technical problems, the technical scheme of the invention is as follows:
the embodiment of the invention provides an operation control method of rocket control software, which comprises the following steps:
acquiring a voice control instruction input through voice input equipment;
analyzing the voice control instruction to obtain a voice characteristic signal corresponding to the voice control instruction;
if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction;
and carrying out operation control on the rocket control software according to the operation.
Optionally, analyzing the voice control instruction to obtain a voice feature signal corresponding to the voice control instruction includes:
carrying out digital conversion processing on the voice control instruction to obtain a digital signal of the voice control instruction;
and converting the digital signal from a time domain to a frequency domain to obtain a voice characteristic signal corresponding to the voice control instruction.
Optionally, if the voice feature signal is successfully matched with the preset voice data, determining an operation corresponding to the voice control instruction, including:
and if the voice characteristic signal is successfully matched with the first preset voice data, determining the operation authority as an administrator authority, logging in the rocket control software according to the voice control instruction, and modifying and/or deleting the flow instruction of the rocket control software.
Optionally, if the voice feature signal is successfully matched with the preset voice data, determining an operation corresponding to the voice control instruction, including:
and converting the voice characteristic signal into a first text instruction, if the first text instruction is successfully matched with a text corresponding to second preset voice data, determining that the operation authority is a common user authority, and browsing the rocket control software according to the voice control instruction.
Optionally, if the voice feature signal is successfully matched with the preset voice data, determining an operation corresponding to the voice control instruction, including:
converting the voice characteristic signal into a second text instruction;
and if the second text instruction is successfully matched with the text corresponding to the third preset voice data, starting a target process of the rocket control software.
Optionally, after starting the target process of the rocket control software, the method further includes:
acquiring a voice flow instruction corresponding to at least one flow instruction input by voice input equipment;
and controlling the rocket control software to execute the flow instruction of the target flow according to the voice flow instruction.
Optionally, controlling the rocket control software to execute the flow instruction of the target flow according to the voice flow instruction includes:
converting the voice flow instruction into a third text instruction;
and if the third text instruction is matched with the target flow instruction of the target flow, controlling the rocket control software to execute the target flow instruction.
An embodiment of the present invention further provides an operation control device of rocket control software, including:
the acquisition module is used for acquiring a voice control instruction input through the voice input equipment;
the processing module is used for analyzing the voice control instruction to obtain a voice characteristic signal corresponding to the voice control instruction; if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction; and carrying out operation control on the rocket control software according to the operation.
Embodiments of the present invention also provide a computing device, comprising: a processor, and a memory storing a computer program that, when executed by the processor, executes the operation control method of the rocket control software.
Embodiments of the present invention also provide a computer-readable storage medium including instructions that, when executed on a computer, cause the computer to execute the operation control method of the rocket control software described above.
The scheme of the invention at least comprises the following beneficial effects:
the scheme of the invention obtains the voice control instruction input by the voice input equipment; analyzing the voice control instruction to obtain a voice characteristic signal corresponding to the voice control instruction; if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction; and carrying out operation control on the rocket control software according to the operation. The remote control of the rocket control software is realized, so that the operation of the rocket control software is more convenient and faster, and the use threshold of the rocket control software is reduced.
Drawings
FIG. 1 is a flow chart illustrating a method for controlling the operation of rocket control software according to the present invention;
FIG. 2 is a schematic view showing a login flow in the operation control method of the rocket control software of the present invention;
FIG. 3 is a flow chart illustrating the execution of the operational control method of the rocket control software according to the present invention;
FIG. 4 is a block diagram of the operational control means of the rocket control software of the present invention.
Detailed Description
Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art.
As shown in fig. 1, an embodiment of the present invention provides an operation control method of rocket control software, including:
step 11, acquiring a voice control instruction input by a voice input device;
step 12, analyzing the voice control instruction to obtain a voice characteristic signal corresponding to the voice control instruction;
step 13, if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction;
and 14, operating and controlling the rocket control software according to the operation.
In the embodiment, in the using process, a device for converting the words by voice, a keyword retrieval function and a function of executing an instruction after voice recognition are added in software; when the rocket control software is used, the audio frequency of a voice control instruction input by voice input equipment (such as a microphone) is used for extracting keywords, then the extracted keywords are subjected to signal processing to realize character conversion, and the instruction after the character conversion corresponds to a step to be executed in the software, so that the rocket control software is operated and controlled through voice; by the method, an operator can still realize accurate control over the rocket control software under the condition that the operator is unfamiliar with the positions corresponding to the flow keys, the use threshold of the software is reduced, the condition of clicking errors possibly occurring during manual operation in the prior art is avoided, remote control over the rocket control software is realized, and the operation of the rocket control software is more convenient and faster.
In an alternative embodiment of the present invention, step 12 may comprise:
step 121, performing digital conversion processing on the voice control instruction to obtain a digital signal of the voice control instruction;
and step 122, converting the digital signal from a time domain to a frequency domain to obtain a voice characteristic signal corresponding to the voice control instruction.
In this embodiment, after the voice input device receives the voice control instruction, the voice input device converts an analog signal of the voice control instruction into a digital signal through sampling processing, then a voice processing module in the rocket control software performs feature extraction on the digital signal, extracts a time domain waveform of the voice control instruction through a voice feature sequence which changes with time in a voice waveform of the voice control instruction, converts the time domain waveform of the voice control instruction into a frequency domain waveform, acquires the corresponding voice feature signal of the voice control instruction through the frequency domain waveform, then finally converts the voice feature signal into a text corresponding to the voice feature signal through pattern matching by using the extracted feature vector, and then the rocket control software extracts a keyword in the text by recognizing text content, acquires a corresponding instruction according to the keyword, and opens a flow in the rocket control software according to the corresponding instruction.
In an alternative embodiment of the present invention, step 13 may include:
and 131, if the voice characteristic signal is successfully matched with the first preset voice data, determining that the operation authority is an administrator authority, logging in the rocket control software according to the voice control instruction, and modifying and/or deleting the flow instruction for the rocket control software.
Step 132, converting the voice characteristic signal into a first text instruction, if the first text instruction is successfully matched with a text corresponding to second preset voice data, determining that the operation authority is a common user authority, and browsing the rocket control software according to the voice control instruction.
In this embodiment, a voiceprint recognition device may be added to the software login interface during use, and a user may log in the interface through a specified sentence or a pre-recorded audio recognition. By the method, the distinction between the login of an administrator and the login of a common user can be realized, and the confidentiality of software is improved;
before the software is used, an administrator can record own voice into the software in a mode of registering in advance and stores the voice as first preset voice data, when the administrator logs in, the software matches the currently acquired voice characteristic signal with the first preset voice data, if the matching is successful, the authority of the administrator can be acquired, and then the administrator can log in the rocket control software according to the voice control instruction and modify and/or delete the process instruction of the rocket control software.
Before the software is used, a common user can set second preset voice data in the software in advance, then the software can convert the second preset voice data into a text corresponding to the second preset voice data and store the text in the software, when the common user logs in, the software can convert a currently acquired voice characteristic signal into a first text instruction and match the first text instruction with the text corresponding to the second preset voice data, if the matching is successful, the common user authority can be acquired, then the common user can log in the rocket control software according to the voice control instruction and browse the rocket control software. For example, the user speaks: when the rocket control software receives a voice control instruction of 'seeing the current rocket running state' through a microphone, the rocket control software converts the voice control instruction into a corresponding text, extracts a keyword 'running state', calls a corresponding instruction according to the keyword 'running state', and opens a running state interface in the software through the corresponding instruction.
In an optional embodiment of the present invention, step 13 may further include:
step 133, converting the voice feature signal into a second text instruction;
and step 134, if the second text instruction is successfully matched with the text corresponding to the third preset voice data, starting a target process of the rocket control software.
In this embodiment, the text corresponding to the third preset voice data may be a start instruction, when an administrator or a general user needs to run a target process after logging in software, a voice control instruction required by the target process needs to be sent, then the rocket control software converts the voice characteristic signal corresponding to the voice control instruction into a second text instruction, that is, a required start instruction, and if the second text instruction is successfully matched with the text corresponding to the third preset voice data, the target process of the rocket control software is started.
In an optional embodiment of the present invention, after starting the target process of the rocket control software, the method further includes:
step 135, acquiring a voice flow instruction corresponding to at least one flow instruction input by the voice input device;
and step 136, controlling the rocket control software to execute the flow instruction of the target flow according to the voice flow instruction.
Wherein step 136 may comprise:
step 3161, converting the voice flow instruction into a third text instruction;
step 3162, if the third text instruction matches with the target flow instruction of the target flow, controlling the rocket control software to execute the target flow instruction.
In this embodiment, the rocket control software may control an execution process of the rocket control software through a voice flow instruction in an operation process, for example, when an operation state is abnormal, a user may send a voice flow instruction of "terminate the flow", and the rocket control software may directly terminate the flow after receiving the corresponding voice flow instruction.
The following will exemplify the specific flow of the method of the present invention by taking the case that the rocket control software needs to execute the ground-based integrated power-up flow:
the ground integrated power-up process comprises the steps of ground power supply parameter setting, ground power supply output control, leakage inspection, power supply distribution and the like;
as shown in fig. 2 and fig. 3, firstly, an administrator or a general user logs in a software control interface through a voice verification mode, and then sends out a voice control instruction: the method comprises the steps of 'executing power supply power up', converting an analog signal of a voice control instruction into a digital signal after a microphone receives a corresponding voice control instruction, converting the digital signal into a frequency domain from a time domain by a voice processing module in rocket control software, acquiring a voice characteristic signal corresponding to the voice control instruction, then converting the voice control instruction into a text form through noise reduction processing, and inputting the text form into the rocket control software, extracting key information 'power supply power up' after the software receives the 'executing power supply power up instruction' to acquire a power supply power up instruction, then opening a power supply power up flow prepared in advance according to the power supply power up instruction, loading the power supply power up flow to an interface, simultaneously opening a display interface of a power supply, inquiring whether a user executes the flow, starting to execute the flow according to the steps of 'ground power supply parameter setting', 'ground power supply output control', 'leakage inspection' and 'power supply distribution', and stopping the flow when an operation state is abnormal, wherein in the execution process, the user can stop the flow through the voice flow instruction, for example, the user can directly say 'stop the flow', after the rocket control software receives the corresponding voice control instruction.
An embodiment of the present invention further provides an operation control device 40 of rocket control software, including:
an obtaining module 41, configured to obtain a voice control instruction input through a voice input device;
the processing module 42 is configured to analyze the voice control instruction to obtain a voice feature signal corresponding to the voice control instruction; if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction; and carrying out operation control on the rocket control software according to the operation.
Optionally, analyzing the voice control instruction to obtain a voice feature signal corresponding to the voice control instruction includes:
carrying out digital conversion processing on the voice control instruction to obtain a digital signal of the voice control instruction;
and converting the digital signal from a time domain to a frequency domain to obtain a voice characteristic signal corresponding to the voice control instruction.
Optionally, if the voice feature signal is successfully matched with the preset voice data, determining an operation corresponding to the voice control instruction, including:
and if the voice characteristic signal is successfully matched with the first preset voice data, determining the operation authority as an administrator authority, logging in the rocket control software according to the voice control instruction, and modifying and/or deleting the flow instruction of the rocket control software.
Optionally, if the voice feature signal is successfully matched with the preset voice data, determining an operation corresponding to the voice control instruction, including:
and converting the voice characteristic signal into a first text instruction, if the first text instruction is successfully matched with a text corresponding to second preset voice data, determining that the operation authority is a common user authority, and browsing the rocket control software according to the voice control instruction.
Optionally, if the voice feature signal is successfully matched with the preset voice data, determining an operation corresponding to the voice control instruction, including:
converting the voice characteristic signal into a second text instruction;
and if the second text instruction is successfully matched with the text corresponding to the third preset voice data, starting a target process of the rocket control software.
Optionally, after starting the target process of the rocket control software, the method further includes:
acquiring a voice flow instruction corresponding to at least one flow instruction input by voice input equipment;
and controlling the rocket control software to execute the flow instruction of the target flow according to the voice flow instruction.
Optionally, controlling the rocket control software to execute the flow instruction of the target flow according to the voice flow instruction includes:
converting the voice flow instruction into a third text instruction;
and if the third text instruction is matched with the target flow instruction of the target flow, controlling the rocket control software to execute the target flow instruction.
It should be noted that the apparatus is an apparatus corresponding to the operation control method of the rocket control software, and all implementation manners in the method are applicable to the embodiment of the apparatus, and the same technical effect can be achieved.
Embodiments of the present invention also provide a computing device, comprising: a processor, and a memory storing a computer program that, when executed by the processor, executes the operation control method of the rocket control software. All the implementation manners in the above method embodiment are applicable to this embodiment, and the same technical effect can be achieved.
Embodiments of the present invention also provide a computer-readable storage medium including instructions that, when executed on a computer, cause the computer to execute the above-described operation control method of the rocket control software. All the implementation manners in the above method embodiments are applicable to the embodiment, and the same technical effect can be achieved.
Those of ordinary skill in the art will appreciate that the various illustrative elements and algorithm steps described in connection with the embodiments disclosed herein may be implemented as electronic hardware, or combinations of computer software and electronic hardware. Whether such functionality is implemented as hardware or software depends upon the particular application and design constraints imposed on the implementation. Skilled artisans may implement the described functionality in varying ways for each particular application, but such implementation decisions should not be interpreted as causing a departure from the scope of the present invention.
It is clear to those skilled in the art that, for convenience and brevity of description, the specific working processes of the above-described systems, apparatuses and units may refer to the corresponding processes in the foregoing method embodiments, and are not described herein again.
In the embodiments provided in the present invention, it should be understood that the disclosed apparatus and method may be implemented in other ways. For example, the above-described apparatus embodiments 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.
The units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the units can be selected according to actual needs to achieve the purpose of the solution of the embodiment.
In addition, functional units in the embodiments of the present invention may be integrated into one processing unit, or each unit may exist alone physically, or two or more units are integrated into one unit.
The functions, if implemented in the form of software functional units and sold or used as a stand-alone product, may be stored in a computer readable storage medium. Based on such understanding, the technical solution of the present invention may be embodied in the form of a software product, which is stored in a storage medium and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device) to execute all or part of the steps of the method according to the embodiments of the present invention. And the aforementioned storage medium includes: various media capable of storing program codes, such as a U disk, a removable hard disk, a ROM, a RAM, a magnetic disk, or an optical disk.
Furthermore, it is to be noted that in the device and method of the invention, it is obvious that the individual components or steps can be decomposed and/or recombined. These decompositions and/or recombinations are to be regarded as equivalents of the present invention. Also, the steps of performing the series of processes described above may naturally be performed chronologically in the order described, but need not necessarily be performed chronologically, and some steps may be performed in parallel or independently of each other. It will be understood by those skilled in the art that all or any of the steps or elements of the method and apparatus of the present invention may be implemented in any computing device (including processors, storage media, etc.) or network of computing devices, in hardware, firmware, software, or any combination thereof, which can be implemented by those skilled in the art using their basic programming skills after reading the description of the present invention.
Thus, the objects of the invention may also be achieved by running a program or a set of programs on any computing device. The computing device may be a general purpose device as is well known. The object of the invention is thus also achieved solely by providing a program product comprising program code for implementing the method or the apparatus. That is, such a program product also constitutes the present invention, and a storage medium storing such a program product also constitutes the present invention. It is to be understood that the storage medium may be any known storage medium or any storage medium developed in the future. It is also noted that in the apparatus and method of the present invention, it is apparent that each component or step can be decomposed and/or recombined. These decompositions and/or recombinations are to be considered as equivalents of the present invention. Also, the steps of executing the series of processes described above may naturally be executed chronologically in the order described, but need not necessarily be executed chronologically. Some steps may be performed in parallel or independently of each other.
While the foregoing is directed to the preferred embodiment of the present invention, it will be understood by those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention as defined in the appended claims.

Claims (10)

1. An operation control method of rocket control software, comprising:
acquiring a voice control instruction input through voice input equipment;
analyzing the voice control instruction to obtain a voice characteristic signal corresponding to the voice control instruction;
if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction;
and carrying out operation control on the rocket control software according to the operation.
2. A method for controlling operation of rocket control software according to claim 1, wherein analyzing the voice control command to obtain a voice feature signal corresponding to the voice control command comprises:
carrying out digital conversion processing on the voice control instruction to obtain a digital signal of the voice control instruction;
and converting the digital signal from a time domain to a frequency domain to obtain a voice characteristic signal corresponding to the voice control instruction.
3. The method of claim 2, wherein if the voice feature signal matches the predetermined voice data successfully, determining the operation corresponding to the voice control command comprises:
and if the voice characteristic signal is successfully matched with the first preset voice data, determining the operation authority as an administrator authority, logging in the rocket control software according to the voice control instruction, and modifying and/or deleting the flow instruction of the rocket control software.
4. The method of claim 2, wherein if the voice feature signal matches the predetermined voice data successfully, determining the operation corresponding to the voice control command comprises:
and converting the voice characteristic signal into a first text instruction, if the first text instruction is successfully matched with a text corresponding to second preset voice data, determining that the operation authority is a common user authority, and browsing the rocket control software according to the voice control instruction.
5. The method of claim 2, wherein if the voice feature signal is successfully matched with predetermined voice data, determining an operation corresponding to the voice control command comprises:
converting the voice characteristic signal into a second text instruction;
and if the second text instruction is successfully matched with the text corresponding to the third preset voice data, starting a target process of the rocket control software.
6. A method for controlling operation of rocket control software according to claim 5, wherein after starting said target process of rocket control software, further comprising:
acquiring a voice flow instruction corresponding to at least one flow instruction input by voice input equipment;
and controlling the rocket control software to execute the flow instruction of the target flow according to the voice flow instruction.
7. A method for controlling operation of rocket control software according to claim 6, wherein controlling said rocket control software to execute said flow instructions of said target flow according to said voice flow instructions comprises:
converting the voice flow instruction into a third text instruction;
and if the third text instruction is matched with the target flow instruction of the target flow, controlling the rocket control software to execute the target flow instruction.
8. An operation control device of rocket control software, comprising:
the acquisition module is used for acquiring a voice control instruction input through the voice input equipment;
the processing module is used for analyzing the voice control instruction to obtain a voice characteristic signal corresponding to the voice control instruction; if the voice characteristic signal is successfully matched with preset voice data, determining the operation corresponding to the voice control instruction; and carrying out operation control on the rocket control software according to the operation.
9. A computing device, comprising: a processor, a memory storing a computer program which, when executed by the processor, performs the method of any of claims 1 to 7.
10. A computer-readable storage medium storing instructions that, when executed on a computer, cause the computer to perform the method of any one of claims 1 to 7.
CN202310010254.0A 2023-01-05 2023-01-05 Operation control method, device and equipment of rocket control software Pending CN115933501A (en)

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Application Number Priority Date Filing Date Title
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Citations (6)

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Publication number Priority date Publication date Assignee Title
CN104570835A (en) * 2014-12-02 2015-04-29 苏州长风航空电子有限公司 Cockpit voice command control system and operating method thereof
CN108122553A (en) * 2017-12-20 2018-06-05 深圳市道通智能航空技术有限公司 A kind of unmanned aerial vehicle (UAV) control method, apparatus, remote control equipment and UAV system
CN110555295A (en) * 2018-06-01 2019-12-10 通用电气航空***有限公司 system and method for reliable command in a vehicle
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CN111833868A (en) * 2020-06-30 2020-10-27 北京小米松果电子有限公司 Voice assistant control method, device and computer readable storage medium
CN113393836A (en) * 2021-06-08 2021-09-14 成都傅立叶电子科技有限公司 Airborne station voice recognition control method and system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104570835A (en) * 2014-12-02 2015-04-29 苏州长风航空电子有限公司 Cockpit voice command control system and operating method thereof
CN108122553A (en) * 2017-12-20 2018-06-05 深圳市道通智能航空技术有限公司 A kind of unmanned aerial vehicle (UAV) control method, apparatus, remote control equipment and UAV system
CN110555295A (en) * 2018-06-01 2019-12-10 通用电气航空***有限公司 system and method for reliable command in a vehicle
US20200005661A1 (en) * 2018-06-27 2020-01-02 Cubic Corporation Phonic fires trainer
CN111833868A (en) * 2020-06-30 2020-10-27 北京小米松果电子有限公司 Voice assistant control method, device and computer readable storage medium
CN113393836A (en) * 2021-06-08 2021-09-14 成都傅立叶电子科技有限公司 Airborne station voice recognition control method and system

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