WO2024230829A1 - Multi-task scheduling management method and apparatus, and device and storage medium - Google Patents

Abstract

Provided in the embodiments of the present application are a multi-task scheduling management method and apparatus, and a device and a storage medium. The method comprises: acquiring reconnaissance data sent by a reconnaissance aircraft; determining task aircraft information of a plurality of task aircrafts, wherein the task aircraft information comprises the current position, endurance mileage, task aircraft type and task arrangement information of each task aircraft; determining a target task aircraft from among the plurality of task aircrafts according to the reconnaissance data and the task aircraft information of the plurality of task aircrafts; and determining flight information of the target task aircraft according to the reconnaissance data, and sending flight information to the target task aircraft, wherein the flight information comprises a flight path and a task instruction. By means of the method, the task execution efficiency is improved.

Description

Multi-task scheduling management method, device, equipment and storage medium Technical Field

The present application belongs to the field of communication technology, and specifically relates to a multi-task scheduling management method, device, equipment and storage medium.

Background Art

The scheduling of UAV swarm tasks needs to consider the requirements of the UAV’s own tasks, as well as the constraints of the coordinated execution of tasks by multiple UAVs, and design collaborative flight missions for multiple UAVs based on task planning.

In the prior art, the scheduling of drone swarm tasks often involves manual input of scheduling tasks, which greatly reduces work efficiency and introduces human errors, resulting in low efficiency of task execution.

Summary of the invention

The embodiments of the present application relate to a multi-task scheduling management method, apparatus, device and storage medium, which are used to solve the defect of low efficiency of drone cluster task execution in the prior art.

In a first aspect, an embodiment of the present application provides a multi-task scheduling management method, including:

Obtain reconnaissance data sent by reconnaissance aircraft;

Determine mission aircraft information of multiple mission aircraft, wherein the mission aircraft information includes current location, mileage, mission aircraft type and mission arrangement information of the mission aircraft;

Determine a target mission machine from among the plurality of mission machines according to the reconnaissance data and mission machine information of the plurality of mission machines;

The flight information of the target mission aircraft is determined according to the reconnaissance data, and the flight information is sent to the target mission aircraft, wherein the flight information includes a flight trajectory and mission instructions.

In a possible implementation, determining a target mission machine from among the multiple mission machines according to the reconnaissance data and the mission machine information of the multiple mission machines includes:

Determine the reconnaissance mission and the mission information of the reconnaissance mission according to the reconnaissance data. The task information includes the task type, task execution period and task execution location;

The target task machine is determined from among the plurality of task machines according to the task information and the task machine information of the plurality of task machines.

In a possible implementation manner, determining the target task machine from the multiple task machines according to the task information and the task machine information of the multiple task machines includes:

For any task machine, determine the idle time period of the task machine according to the task arrangement information of the task machine;

Determine at least one task machine to be selected from the plurality of task machines according to the idle periods of the plurality of task machines and the task execution period;

The target task machine is determined from the at least one task machine to be selected according to the task type, the task execution location, and the task machine information of each task machine to be selected.

In a possible implementation, determining the target task machine from the at least one candidate task machine according to the task type, the task execution location, and the task machine information of each candidate task machine includes:

According to the task type and the task machine type of each candidate task machine, determining at least one first task machine from the at least one candidate task machine, wherein the task machine type of the first task machine matches the task type;

If the number of the first task machine is 1, the first task machine is determined as the target task machine;

If the number of the first task machines is greater than 1, the target task machine is determined from the at least one first task machine according to the task execution position, and the current position and cruising range of each first task machine.

In a possible implementation, determining the target mission machine in the at least one first mission machine according to the mission execution position, and the current position and cruising range of each first mission machine includes:

Determine the reconnaissance flight mileage corresponding to the reconnaissance mission;

Determining the empty flight mileage according to the mission execution location and the current location of each first mission aircraft;

The target mission aircraft is determined from the at least one first mission aircraft according to the reconnaissance flight mileage, the air flight mileage and the cruising range, and the cruising range of the target mission aircraft is greater than the sum of the reconnaissance flight mileage and the air flight mileage.

In a possible implementation, the reconnaissance mission includes at least one of the following: a rescue mission, a driving mission, or a relay communication mission.

In a possible implementation, obtaining the reconnaissance data sent by the reconnaissance aircraft includes:

receiving the reconnaissance data sent by the reconnaissance aircraft; or,

The reconnaissance data sent by the relay device is received, where the reconnaissance data is data sent by the reconnaissance aircraft to the relay device.

In a second aspect, an embodiment of the present application provides a multi-task scheduling management device, including:

An acquisition module is used to acquire the reconnaissance data sent by the reconnaissance aircraft;

A first determination module is used to determine the mission aircraft information of multiple mission aircraft, wherein the mission aircraft information includes the current position, mileage, mission aircraft type and mission arrangement information of the mission aircraft;

A second determination module is used to determine a target mission machine from among the multiple mission machines according to the reconnaissance data and the mission machine information of the multiple mission machines;

A third determination module is used to determine the flight information of the target mission aircraft according to the reconnaissance data;

The sending module is used to send the flight information to the target mission aircraft, and the flight information includes a flight trajectory and mission instructions.

In a possible implementation manner, the second determining module is specifically configured to:

Determine a reconnaissance mission and mission information of the reconnaissance mission according to the reconnaissance data, wherein the mission information includes a mission type, a mission execution period, and a mission execution location;

The target task machine is determined from among the plurality of task machines according to the task information and the task machine information of the plurality of task machines.

In a possible implementation manner, the second determining module is specifically configured to:

For any task machine, determine the idle time period of the task machine according to the task arrangement information of the task machine;

Determine at least one task machine to be selected from the plurality of task machines according to the idle periods of the plurality of task machines and the task execution period;

The target task machine is determined from the at least one task machine to be selected according to the task type, the task execution location, and the task machine information of each task machine to be selected.

In a possible implementation manner, the second determining module is specifically configured to:

According to the task type and the task machine type of each candidate task machine, at least one first task machine is determined in the at least one candidate task machine, and the task machine type of the first task machine is the same as the task machine type of the Match the task type;

If the number of the first task machine is 1, the first task machine is determined as the target task machine;

If the number of the first task machines is greater than 1, the target task machine is determined from the at least one first task machine according to the task execution position, and the current position and cruising range of each first task machine.

In a possible implementation manner, the second determining module is specifically configured to:

Determine the reconnaissance flight mileage corresponding to the reconnaissance mission;

Determining the empty flight mileage according to the mission execution location and the current location of each first mission aircraft;

The target mission aircraft is determined from the at least one first mission aircraft according to the reconnaissance flight mileage, the air flight mileage and the cruising range, and the cruising range of the target mission aircraft is greater than the sum of the reconnaissance flight mileage and the air flight mileage.

In a possible implementation, the reconnaissance mission includes at least one of the following: a rescue mission, a driving mission, or a relay communication mission.

In a possible implementation, the acquisition module is specifically used to:

receiving the reconnaissance data sent by the reconnaissance aircraft; or,

The reconnaissance data sent by the relay device is received, where the reconnaissance data is data sent by the reconnaissance aircraft to the relay device.

In a third aspect, an embodiment of the present application provides a multi-task scheduling management device, including: a memory and a processor;

The memory stores computer-executable instructions;

The processor executes the computer-executable instructions stored in the memory to implement the multi-task scheduling management method as described in any one of the first aspects.

In a fourth aspect, an embodiment of the present application provides a computer-readable storage medium, wherein the computer-readable storage medium stores computer execution instructions, which, when executed by a processor, are used to implement the multi-task scheduling management method described in any one of the first aspects.

In a fifth aspect, an embodiment of the present application provides a computer program product, including a computer program, which, when executed by a processor, implements the multi-task scheduling management method described in any one of the first aspects.

The present invention provides a multi-task scheduling management method, device, equipment and storage medium. In the method, the reconnaissance data sent by the reconnaissance aircraft is obtained; the mission aircraft information of multiple mission aircraft is determined, and the mission aircraft information includes the current position, cruising range, mission aircraft type and mission arrangement information of the mission aircraft; the target mission aircraft is determined from the multiple mission aircraft according to the reconnaissance data and the mission aircraft information of the multiple mission aircraft; the flight information of the target mission aircraft is determined according to the reconnaissance data, and the flight information is sent to the target mission aircraft, and the flight information includes the flight trajectory and mission instructions. In this way, the target mission aircraft that best meets the conditions for executing the mission instructions can be selected from multiple mission aircraft quickly and accurately, and the mission scheduling is intelligent, and multiple reconnaissance aircraft reconnaissance and multiple mission aircraft execution are realized. Moreover, the mission aircraft can execute the mission instructions according to the flight trajectory planned by the multi-task scheduling system, avoiding collisions between mission aircraft due to the same planned routes, and avoiding errors caused by human scheduling, thereby improving the efficiency of mission execution.

BRIEF DESCRIPTION OF THE DRAWINGS

In order to more clearly illustrate the technical solutions in the present application, a brief introduction will be given below to the drawings required for use in the description of the embodiments. Obviously, the drawings described below are some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

FIG1 is a schematic diagram of an application scenario provided by an embodiment of the present application;

FIG2 is a flow chart of a multi-task scheduling management method provided in an embodiment of the present application;

FIG3 is a flow chart of another multi-task scheduling management method provided in an embodiment of the present application;

FIG4 is a schematic diagram of the structure of a multi-task scheduling management device provided in an embodiment of the present application;

FIG5 is a schematic diagram of the structure of an electronic device provided in an embodiment of the present application.

The above drawings have shown clear embodiments of the present application, which will be described in more detail later. These drawings and text descriptions are not intended to limit the scope of the present application in any way, but to illustrate the concept of the present application to those skilled in the art by referring to specific embodiments.

DETAILED DESCRIPTION

In order to make the purpose, technical solution and advantages of the embodiments of the present application clearer, the technical solution in the embodiments of the present application will be described clearly and completely in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, ordinary technicians in this field can obtain the above-mentioned results without creative work. All other embodiments obtained are within the scope of protection of this application.

It should be noted that, although the terms "first", "second", etc. are used to describe various information in the embodiments of the present application, such information should not be limited to these terms. These terms are only used to distinguish the same type of information from each other. Optionally, without departing from the scope of the present application, the first information may also be referred to as the second information, and similarly, the second information may also be referred to as the first information.

It should be understood that the terms "comprises" and "includes" indicate the presence of the previously mentioned features, steps, operations, but do not exclude the presence, occurrence or addition of one or at least one other feature, step, operation. The terms "and/or" and the like used in this application may be interpreted as inclusive, or mean any one or any combination. Optionally, "A and/or B" means "any of the following: A; B; A and B". In addition, the character "/" in this article generally indicates that the objects associated before and after are in an "or" relationship.

In the prior art, the scheduling of drone clusters requires manual input of scheduling tasks, which has low work efficiency and may introduce human errors, resulting in low accuracy of task execution.

In order to solve the above technical problems, the embodiment of the present application provides a schematic diagram of an application scenario, see Figure 1. The application scenario of the present application includes: multiple reconnaissance aircraft 101, a server 102, and multiple mission machines 103. The server 102 can be wirelessly connected with multiple reconnaissance aircraft 101 and multiple mission machines 103.

Among them, the reconnaissance aircraft 101 can be an aircraft with long range, high altitude, high speed and detection, which can be used to detect ground conditions from the air, and can also be equipped with different sensors to achieve professional performance. For example, the reconnaissance aircraft can be equipped with infrared sensors and thermal imaging sensors, so that the reconnaissance aircraft can detect ground conditions in a dark environment. The reconnaissance aircraft 101 can include rotorcraft, fixed-wing aircraft, Electric Vertical Takeoff and Landing (EVTOL) aircraft, etc.

The server 102 can provide a scheduling management service for multiple task machines 103. The server 102 can be a cloud server, a server of a distributed system, or a server combined with a blockchain. A multi-task scheduling management system can be deployed in the server 102. The multi-task scheduling management system supports obtaining the reconnaissance situation of multiple reconnaissance aircraft and analyzing the reconnaissance situation.

The multiple mission machines 103 may be different types of mission machines. The types of mission machines include, but are not limited to, patrol mission machines, transport mission machines, communication mission machines, etc. The multi-task scheduling management system in the server 102 supports scheduling and management of multiple types of mission machines. The mission machines 103 may include rotorcraft, fixed-wing aircraft, electric vertical takeoff and landing (EVTOL) aircraft, etc.

An embodiment of the present application provides a multi-task scheduling management method, which is applied to a multi-task scheduling system. The target task aircraft and the flight information of the target task aircraft are determined through the reconnaissance data sent by the reconnaissance aircraft and the task aircraft information of multiple task aircraft. The flight information includes the flight trajectory and task instructions, so that the target task aircraft executes the task instructions according to the flight trajectory. This avoids the introduction of errors caused by human scheduling, makes task scheduling intelligent, realizes reconnaissance by multiple reconnaissance aircraft, and executes tasks by multiple task aircraft, thereby improving the efficiency of task execution.

The technical solution shown in the present application is described in detail below through specific embodiments. It should be noted that the following embodiments can exist independently or in combination with each other, and the same or similar contents will not be described repeatedly in different embodiments.

FIG2 is a flow chart of a multi-task scheduling management method provided by an embodiment of the present application. The execution subject of the embodiment of the present application can be an electronic device, or a multi-task scheduling management device set in the electronic device. The multi-task scheduling management device can be implemented by software, or by a combination of software and hardware. Referring to FIG2, the method includes:

S201. Acquire reconnaissance data sent by a reconnaissance aircraft.

The reconnaissance data may include the location information of the reconnaissance point and the situation information of the reconnaissance point. The location information may include longitude and latitude information. The situation information may be natural disasters such as sudden fires and landslides, or a person without access rights entering a monitoring area with access rights, or a detection of no communication signals in a certain area, etc., which are not limited here.

The reconnaissance data sent by the reconnaissance aircraft may be obtained in the following manner: receiving the reconnaissance data sent by the reconnaissance aircraft; or receiving the reconnaissance data sent by the relay device, where the reconnaissance data is data sent by the reconnaissance aircraft to the relay device.

The reconnaissance aircraft can obtain reconnaissance data through multiple sensors carried by it, which are not limited here.

S202: Determine task machine information of multiple task machines.

There may be a preset association relationship between the reconnaissance aircraft and the mission aircraft. A reconnaissance aircraft may be associated with one or more mission aircraft. The mission aircraft information of the mission aircraft includes the current location of the mission aircraft, the cruising range, the mission aircraft type and the mission arrangement information, which are not limited here.

Optionally, one or more corresponding mission machine identifiers are determined based on the identifier and association relationship of the reconnaissance aircraft, and mission machine information of the one or more mission machines is determined based on the identifier of the mission machine.

S203. Determine a target mission machine from among the multiple mission machines based on the reconnaissance data and the mission machine information of the multiple mission machines.

The task machine information of the multiple task machines can be determined according to the task information of the multiple task machines, and the reconnaissance task can be determined according to the reconnaissance data. Among the multiple task machines, the target task machine that meets the reconnaissance task can be determined according to the task machine information of the multiple task machines.

S204. Determine the flight information of the target mission aircraft according to the reconnaissance data, and send the flight information to the target mission aircraft.

The reconnaissance mission can be determined based on the reconnaissance data, and the flight information of the target mission aircraft can be determined based on the reconnaissance mission. The flight information may include a flight trajectory and mission instructions. The flight information is sent to the target mission aircraft so that the target mission aircraft can fly according to the flight trajectory and execute the mission instructions, thereby realizing task scheduling.

The multi-task scheduling management method provided in this embodiment obtains the reconnaissance data sent by the reconnaissance aircraft; determines the task aircraft information of multiple task aircraft, the task aircraft information includes the current position of the task aircraft, the cruising range, the task aircraft type and the task arrangement information; determines the target task aircraft among the multiple task aircraft according to the reconnaissance data and the task aircraft information of the multiple task aircraft; determines the flight information of the target task aircraft according to the reconnaissance data, and sends the flight information to the target task aircraft, the flight information includes the flight trajectory and the task instruction. Thus, it is possible to quickly and accurately select the target task aircraft that best meets the conditions for executing the task instruction from multiple task aircraft, make the task scheduling intelligent, realize the reconnaissance of multiple reconnaissance aircraft, and the execution of tasks by multiple task aircraft, and the task aircraft can execute the task instruction according to the flight trajectory planned by the multi-task scheduling system, avoid the collision between the task aircraft due to the same planned route, and avoid the errors caused by the introduction of human scheduling, thereby improving the efficiency of task execution.

FIG3 is a flow chart of a multi-task scheduling management method provided by an embodiment of the present application. Based on the above embodiment, the method can be described in detail with reference to FIG3. The method includes:

S301. Acquire reconnaissance data sent by a reconnaissance aircraft.

The execution process of S301 can refer to the execution process of S201, which will not be described in detail here.

S302: Determine task machine information of multiple task machines.

The execution process of S302 can refer to the execution process of S202, which will not be described in detail here.

S303: Determine the reconnaissance mission and mission information of the reconnaissance mission according to the reconnaissance data.

The task information may include the task type, task execution period, and task execution location.

The reconnaissance mission can be determined based on the reconnaissance data. The reconnaissance mission can include at least one of the following: a rescue mission, a driving mission, or a relay communication mission. The corresponding mission can be determined based on the reconnaissance mission. Machine type.

The mission information of the reconnaissance mission can be determined based on the reconnaissance data. The mission information may include the mission type, mission execution period and mission execution location. Thus, the target mission machine that best meets the mission information can be determined from multiple mission machines associated with the reconnaissance aircraft, thereby improving the efficiency of mission execution.

S304: For any task machine, determine the idle time period of the task machine according to the task scheduling information of the task machine.

Among them, the task scheduling information of all task machines is stored in the multi-task scheduling system. For any task machine, the task scheduling information of the task machine is obtained, and the task execution period and idle period of the task machine are determined according to the task scheduling information, so that at least one task machine that meets the task execution period of the reconnaissance task can be quickly and accurately determined among the multiple task machines associated with the reconnaissance machine.

S305: Determine at least one task machine to be selected from the multiple task machines according to the idle periods and task execution periods of the multiple task machines.

The idle time periods and task execution time periods of multiple task machines associated with the reconnaissance machine are obtained, and at least one task machine to be selected is determined from the multiple task machines according to the idle time periods and task execution time periods of the multiple task machines and the task execution time period of the reconnaissance task. Among them, the task execution time period of the reconnaissance task must not overlap with the task execution time period of the task machine to be selected, and overlap with the idle time period of the task machine to be selected, so as to realize reasonable scheduling between task machines and avoid the task machine being unable to complete the reconnaissance task in time due to other tasks being executed.

S306: Determine at least one first task machine from at least one of the candidate task machines according to the task type and the task machine type of each candidate task machine, wherein the task machine type of the first task machine matches the task type.

According to the task type of the reconnaissance mission and the task machine type of at least one candidate task machine, at least one task machine consistent with the task type of the reconnaissance mission is matched among the at least one candidate task machine, and the task machine is used as the first task machine to avoid the problem of low task execution efficiency caused by different task machine types. The first task machine with consistent task type is determined through the multi-task scheduling management system to improve the task execution efficiency.

At least one first task machine at least meets the following conditions: being in an idle state during a task execution period of the reconnaissance task and matching a task type of the reconnaissance task.

S307: Determine the number of first task machines.

If the number of the first task machine is 1, execute S308.

If the number of the first task machines is greater than 1, execute S309.

S308: Determine the first task machine as the target task machine.

After S308 , S310 is executed.

If the number of the first task machine is 1, the first task machine is directly used as the target task machine.

S309: Determine a target mission machine from at least one first mission machine according to the mission execution location, and the current location and cruising range of each first mission machine.

After S309, S310 is executed.

If the number of first mission aircraft is greater than 1, one of the first mission aircraft can be selected as the target mission aircraft from among the multiple first mission aircraft based on the cruising range being greater than the total mileage required to perform the mission. The target mission aircraft with a cruising range greater than the total mileage required to perform the mission can be determined based on the mission execution location of the reconnaissance mission, the current location of each first mission aircraft, and the cruising range of each first mission aircraft.

The target mission aircraft can be determined in at least one first mission aircraft in the following manner: determine the reconnaissance flight mileage corresponding to the reconnaissance mission; determine the empty flight mileage based on the mission execution location and the current location of each first mission aircraft; determine the target mission aircraft in at least one first mission aircraft based on the reconnaissance flight mileage, empty flight mileage and cruising range, the cruising range of the target mission aircraft being greater than the sum of the reconnaissance flight mileage and the empty flight mileage.

Among them, the reconnaissance flight mileage can be the flight mileage required to complete the reconnaissance mission estimated by the multi-task scheduling system based on the reconnaissance mission. The empty flight mileage can be the shortest mileage from the current position of the mission aircraft to the mission execution position. By estimating the reconnaissance flight mileage through the multi-task scheduling system, the target mission aircraft is determined based on the reconnaissance flight mileage, empty flight mileage and cruising range, and the target mission aircraft that meets the mission execution conditions can be quickly and accurately selected from at least one first mission aircraft, avoiding the situation where the mission aircraft cannot complete the mission execution due to its own cruising range problem, thereby improving the efficiency of mission execution.

S310. Determine the flight information of the target mission aircraft according to the reconnaissance data, and send the flight information to the target mission aircraft.

The execution process of S310 can refer to the execution process of S204, which will not be described in detail here.

The implementation content of each step in the embodiment of the present application can refer to the description of the corresponding steps or operations in the above method embodiment, and repeated content will not be repeated.

The multi-task scheduling management method provided in this embodiment obtains the reconnaissance data sent by the reconnaissance aircraft. According to the information, the task machine information of multiple task machines is determined, and the reconnaissance task and the task information of the reconnaissance task are determined according to the reconnaissance data. For any task machine, the idle period of the task machine is determined according to the task arrangement information of the task machine. According to the idle period and task execution period of multiple task machines, at least one task machine to be selected is determined from multiple task machines. If the number of first task machines is 1, the first task machine is determined as the target task machine; if the number of first task machines is greater than 1, the target task machine is determined in at least one first task machine according to the task execution position, the current position and the cruising range of each first task machine, and the flight information of the target task machine is determined according to the reconnaissance data, and the flight information is sent to the target task machine, and the flight information includes the flight trajectory and the task instruction. Thus, it is possible to quickly and accurately select the target task machine that best meets the conditions for executing the task instruction from multiple task machines, make the task scheduling intelligent, realize the reconnaissance of multiple reconnaissance machines, and the execution of tasks by multiple task machines, and the task machine can execute the task instruction according to the flight trajectory planned by the multi-task scheduling system, avoid the collision between task machines due to the same planned route, and avoid the errors caused by the introduction of human scheduling, and improve the efficiency of task execution.

The technical solution shown in this application is explained below through specific examples.

For example, if a reconnaissance aircraft detects a fire somewhere in a mountainous area, the reconnaissance aircraft is pre-associated with four mission aircraft, namely A, B, C, and D. Among them, mission aircraft A, B, and C are transport mission aircraft and can be used for rescue missions; mission aircraft D is a patrol mission aircraft and can be used for expulsion missions.

The multi-task scheduling system obtains the reconnaissance data sent by the reconnaissance aircraft and confirms the task machine information of the four task machines associated with the reconnaissance aircraft. The task machine information includes the current location of the task machine, the cruising range, the task machine type and the task scheduling information. According to the reconnaissance data, it is determined that the task type is a rescue mission, the execution period of the task is immediate execution, and the task execution location is the longitude and latitude coordinates of the fire area. According to the task scheduling information of each task machine, the idle period of each task machine is determined, among which task machines A, B and D are currently in the idle period, and task machine C is currently in the task execution period. According to the idle periods and task execution periods of the four task machines, task machines A, B and D are determined as the task machines to be selected. According to the task type of the reconnaissance mission being a rescue mission, and the type of the task machines to be selected, task machines A and B are determined as the first task machines that match the task type of the reconnaissance mission. The reconnaissance flight distance corresponding to the reconnaissance mission is determined to be 10 kilometers, the air flight distance from the current position of mission aircraft A to the mission execution location is determined to be 5 kilometers, and the air flight distance from the current position of mission aircraft B to the mission execution location is determined to be 2 kilometers. Among them, the cruising range of mission aircraft A is 13 kilometers, and the cruising range of mission aircraft B is 18 kilometers. If the mileage is less than the sum of the reconnaissance flight mileage and the empty flight mileage, and the endurance mileage of mission aircraft B is greater than the sum of the reconnaissance flight mileage and the empty flight mileage, then mission aircraft B is determined to be the target mission aircraft. Determine the flight trajectory and mission instructions of mission aircraft B based on the reconnaissance data, and send the flight trajectory and mission instructions to mission aircraft B so that mission aircraft B flies according to the flight trajectory and executes the mission instructions. Through the multi-task scheduling system, the target mission aircraft that best meets the conditions for executing the mission instructions can be quickly and accurately selected from multiple mission aircraft, making the mission scheduling intelligent, realizing multi-reconnaissance aircraft reconnaissance, and multi-task aircraft executing tasks. The mission aircraft can execute the mission instructions according to the flight trajectory planned by the multi-task scheduling system, avoiding collisions between mission aircraft due to the same planned routes, and avoiding errors caused by human scheduling, thereby improving the efficiency of mission execution.

FIG4 is a schematic diagram of the structure of a multi-task scheduling management device provided by an embodiment of the present application. Referring to FIG4, the device 400 includes an acquisition module 401, a first determination module 402, a second determination module 403, a third determination module 404 and a sending module 405, wherein:

The acquisition module 401 is used to acquire the reconnaissance data sent by the reconnaissance aircraft;

The first determination module 402 is used to determine the mission aircraft information of multiple mission aircraft, the mission aircraft information including the current location, mileage, mission aircraft type and mission arrangement information of the mission aircraft;

The second determination module 403 is used to determine a target mission machine from among the multiple mission machines according to the reconnaissance data and the mission machine information of the multiple mission machines;

The third determination module 404 is used to determine the flight information of the target mission aircraft according to the reconnaissance data;

The sending module 405 is used to send flight information to the target mission aircraft, and the flight information includes a flight trajectory and mission instructions.

In a possible implementation manner, the second determining module 403 is specifically configured to:

Determine the reconnaissance mission and mission information of the reconnaissance mission according to the reconnaissance data, wherein the mission information includes the mission type, the mission execution period and the mission execution location;

A target task machine is determined from among the plurality of task machines based on the task information and the task machine information of the plurality of task machines.

In a possible implementation manner, the second determining module 403 is specifically configured to:

For any task machine, determine the idle time period of the task machine according to the task scheduling information of the task machine;

Determine at least one task machine to be selected from the plurality of task machines according to the idle periods and task execution periods of the plurality of task machines;

A target task machine is determined from at least one of the candidate task machines according to the task type, the task execution location, and the task machine information of each candidate task machine.

In a possible implementation manner, the second determining module 403 is specifically configured to:

According to the task type and the task machine type of each candidate task machine, at least one first task machine is determined from at least one candidate task machine, and the task machine type of the first task machine matches the task type;

If the number of the first task machine is 1, the first task machine is determined as the target task machine;

If the number of the first mission machines is greater than 1, a target mission machine is determined from at least one first mission machine according to the mission execution location, and the current location and cruising range of each first mission machine.

In a possible implementation manner, the second determining module 403 is specifically configured to:

Determine the reconnaissance flight mileage corresponding to the reconnaissance mission;

Determine the empty flight mileage according to the mission execution location and the current location of each first mission aircraft;

A target mission aircraft is determined from at least one first mission aircraft according to the reconnaissance flight mileage, the empty flight mileage and the endurance mileage, and the endurance mileage of the target mission aircraft is greater than the sum of the reconnaissance flight mileage and the empty flight mileage.

In a possible implementation, the reconnaissance mission includes at least one of the following: a rescue mission, a driving mission, or a relay communication mission.

In a possible implementation, the acquisition module 405 is specifically used to:

Receive reconnaissance data sent by reconnaissance aircraft; or,

Receive reconnaissance data sent by the relay device, where the reconnaissance data is data sent by the reconnaissance aircraft to the relay device.

FIG5 is a schematic diagram of the structure of an electronic device provided in an embodiment of the present application. Referring to FIG5 , the electronic device 500 may include: a memory 501 , a processor 502 , and a transceiver 503 .

The memory 501 is used to store program instructions;

The processor 502 is used to execute the program instructions stored in the memory, so as to enable the electronic device 20 to execute any of the component parameter determination methods shown above.

The transceiver 503 may include: a transmitter and/or a receiver. The transmitter may also be referred to as a transmitter, a transmitter, a transmission port, a transmission interface, or the like, and the receiver may also be referred to as a receiver, a reception port, a reception interface, or the like. Exemplarily, the memory 501, the processor 502, and the transceiver 503 are interconnected via a bus 504.

The embodiment of the present application also provides a computer program product, which can be executed by a processor. When the computer program product is executed, the above-mentioned component parameter determination method can be implemented.

The component parameter determination device, electronic device, computer-readable storage medium and computer program product of the embodiments of the present application can execute the technical solutions shown in the above-mentioned component parameter determination method embodiments. Their implementation principles and beneficial effects are similar and will not be repeated here.

All or part of the steps of the above-mentioned method embodiments can be completed by hardware related to program instructions. The aforementioned program can be stored in a readable memory. When the program is executed, it executes the steps of the above-mentioned method embodiments; and the aforementioned memory (storage medium) includes: read-only memory (ROM), random access memory (RAM), flash memory, hard disk, solid state drive, magnetic tape, floppy disk, optical disc and any combination thereof.

The present application embodiment is described with reference to the flowchart and/or block diagram of the method, device (system) and computer program product according to the present application embodiment. It should be understood that each process and/or box in the flowchart and/or block diagram and the combination of the process and/or box in the flowchart and/or block diagram can be realized by computer program instructions. These computer program instructions can be provided to the processing unit of a general-purpose computer, a special-purpose computer, an embedded processor or other programmable data processing device to produce a machine, so that the instructions executed by the processing unit of the computer or other programmable data processing device produce a device for realizing the function specified in one process or multiple processes in the flowchart and/or one box or multiple boxes in the block diagram.

These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing device to work in a specific manner, so that the instructions stored in the computer-readable memory produce a manufactured product including an instruction device that implements the functions specified in one or more processes in the flowchart and/or one or more boxes in the block diagram.

These computer program instructions may also be loaded onto a computer or other programmable data processing device so that a series of operational steps are executed on the computer or other programmable device to produce a computer-implemented process, whereby the instructions executed on the computer or other programmable device provide steps for implementing the functions specified in one or more processes in the flowchart and/or one or more boxes in the block diagram.

Obviously, those skilled in the art can make various changes and modifications to the embodiments of the present application without departing from the spirit and scope of the present application. This application is intended to include these changes and modifications as long as they fall within the scope of the claims of this application and their equivalents.

Claims (10)

A multi-task scheduling management method, characterized in that it is applied to a multi-task scheduling system, and the method comprises: Obtain reconnaissance data sent by reconnaissance aircraft; Determine mission aircraft information of multiple mission aircraft, wherein the mission aircraft information includes current location, mileage, mission aircraft type and mission arrangement information of the mission aircraft; Determine a target mission machine from among the plurality of mission machines according to the reconnaissance data and mission machine information of the plurality of mission machines; The flight information of the target mission aircraft is determined according to the reconnaissance data, and the flight information is sent to the target mission aircraft, wherein the flight information includes a flight trajectory and mission instructions. The method according to claim 1 is characterized in that determining a target mission machine from among the multiple mission machines based on the reconnaissance data and the mission machine information of the multiple mission machines comprises: Determine a reconnaissance mission and mission information of the reconnaissance mission according to the reconnaissance data, wherein the mission information includes a mission type, a mission execution period, and a mission execution location; The target task machine is determined from among the plurality of task machines according to the task information and the task machine information of the plurality of task machines. The method according to claim 2 is characterized in that, according to the task information and the task machine information of the multiple task machines, determining the target task machine from the multiple task machines comprises: For any task machine, determine the idle time period of the task machine according to the task arrangement information of the task machine; Determine at least one task machine to be selected from the plurality of task machines according to the idle periods of the plurality of task machines and the task execution period; The target task machine is determined from the at least one task machine to be selected according to the task type, the task execution location, and the task machine information of each task machine to be selected. The method according to claim 3 is characterized in that, according to the task type, the task execution location, and the task machine information of each candidate task machine, determining the target task machine from the at least one candidate task machine comprises: According to the task type and the task machine type of each task machine to be selected, in the at least one Determine at least one first task machine from the candidate task machines, wherein the task machine type of the first task machine matches the task type; If the number of the first task machine is 1, the first task machine is determined as the target task machine; If the number of the first task machines is greater than 1, the target task machine is determined from the at least one first task machine according to the task execution position, and the current position and cruising range of each first task machine. The method according to claim 4 is characterized in that, according to the task execution position, and the current position and cruising range of each first task machine, determining the target task machine in the at least one first task machine comprises: Determine the reconnaissance flight mileage corresponding to the reconnaissance mission; Determining the empty flight mileage according to the mission execution location and the current location of each first mission aircraft; The target mission aircraft is determined from the at least one first mission aircraft according to the reconnaissance flight mileage, the air flight mileage and the endurance mileage, and the endurance mileage of the target mission aircraft is greater than the sum of the reconnaissance flight mileage and the air flight mileage. The method according to any one of claims 2 to 5 is characterized in that the reconnaissance mission includes at least one of the following: a rescue mission, a driving mission or a relay communication mission. The method according to any one of claims 1 to 6, characterized in that obtaining the reconnaissance data sent by the reconnaissance aircraft comprises: receiving the reconnaissance data sent by the reconnaissance aircraft; or, The reconnaissance data sent by the relay device is received, where the reconnaissance data is data sent by the reconnaissance aircraft to the relay device. A multi-task scheduling management device, characterized by comprising: An acquisition module is used to acquire the reconnaissance data sent by the reconnaissance aircraft; A first determination module is used to determine the mission aircraft information of multiple mission aircraft, wherein the mission aircraft information includes the current position, mileage, mission aircraft type and mission arrangement information of the mission aircraft; A second determination module is used to determine a target mission machine from among the multiple mission machines according to the reconnaissance data and the mission machine information of the multiple mission machines; A third determination module is used to determine the flight information of the target mission aircraft according to the reconnaissance data; The sending module is used to send the flight information to the target mission aircraft, and the flight information includes a flight trajectory and mission instructions. A multi-task scheduling management device, characterized in that it comprises: a memory, a processor and a transceiver; Wherein, the memory stores computer-executable instructions; The processor executes the computer-executable instructions stored in the memory to implement the multi-task scheduling management method according to any one of claims 1 to 7. A computer-readable storage medium, characterized in that the computer-readable storage medium stores computer-executable instructions, which, when executed by a processor, are used to implement the multi-task scheduling management method as described in any one of claims 1 to 7.