A high-efficiency management and allocation system for low-altitude aircraft

Abstract

The present invention discloses a high-efficiency management and allocation system for low-altitude aircraft, which belongs to the field of low-altitude aircraft management, including: obtaining flight mission information through a mission receiving module and transmitting it to a mission priority evaluation module, generating a mission priority sequence according to evaluation rules; a charging management module comparing the aircraft power with the power required for the mission in real time, generating a charging demand list, and formulating a charging strategy; if the sudden mission response module receives a sudden mission, the mission priority evaluation module will generate a sudden mission priority, and the aircraft corresponding to the high-priority sudden mission can jump the queue for charging or perform the mission; the status monitoring module provides real-time feedback on the aircraft status, and dynamically adjusts the mission priority sequence and charging strategy, thereby realizing efficient management of low-altitude aircraft, improving utilization efficiency, and ensuring flight safety.

Description

Technical Field

[0001] The present invention relates to the field of low-altitude aircraft management, and more specifically to a high-efficiency management and distribution system for low-altitude aircraft. Background Art

[0002] In practical applications, numerous low-altitude aircraft are required to perform different missions. The challenges of rationally scheduling these missions and managing their power to ensure efficient charging without exceeding safety thresholds, while also addressing emergencies, are pressing. Existing technologies for aircraft mission scheduling and charging management often lack dynamic adjustment capabilities, making them unable to effectively address emergencies or charging resource constraints. This results in inefficient mission execution and can even pose safety risks.

[0003] For example, a Chinese patent with authorization publication number CN106886423B discloses a method and apparatus for distributing loadable software aircraft parts (LSAPs). The software aircraft part management apparatus includes: a library, a receiving module, a proxy server, an onboard electronic distribution system on an aircraft, and a portable software maintenance tool. The library on a ground data processing system stores and manages software aircraft parts for an aircraft. The receiving module is capable of receiving software aircraft parts from suppliers and sending the software aircraft parts to the library. The proxy server communicates with the library and is capable of distributing software to multiple aircraft client systems. The onboard electronic distribution system is an aircraft client system and is capable of receiving software aircraft parts for an aircraft from the library through the proxy server. The portable software maintenance tool provides an alternative way to send software aircraft parts to the onboard electronic distribution system of an aircraft.

[0004] The above existing technologies have the following problems: they only cover the reception, storage, distribution and maintenance of software aircraft components, and do not involve key aspects such as aircraft mission planning, priority determination and power management. They are unable to achieve comprehensive management and optimization of aircraft operations, and it is difficult to ensure the efficient operation of aircraft when performing various tasks; they lack task orientation and have no response mechanism for sudden tasks. When an emergency task arises that needs to be executed first, the allocation strategy of software components cannot be adjusted in time. Summary of the Invention

[0005] In response to the shortcomings of the existing technology, the present invention proposes a high-efficiency management and allocation system for low-altitude aircraft, which obtains flight mission information through the task receiving module and transmits it to the task priority evaluation module, and generates a task priority sequence according to the evaluation rules; the charging management module compares the aircraft power with the power required for the mission in real time, generates a charging demand list, and formulates a charging strategy; if the emergency task response module receives a sudden task, the task priority evaluation module will generate a sudden task priority, and the aircraft corresponding to the high-priority sudden task can jump the queue for charging or perform the task; the status monitoring module provides real-time feedback on the aircraft status, and dynamically adjusts the task priority sequence and charging strategy, thereby realizing efficient management of low-altitude aircraft, improving utilization efficiency, and ensuring flight safety.

[0006] To achieve the above object, the present invention provides the following technical solutions:

[0007] A high-efficiency management and allocation system for low-altitude aircraft, comprising: a task receiving module, a task priority assessment module, a charging management module, and an emergency task response module;

[0008] The mission receiving module obtains the flight mission information of the aircraft and transmits it to the mission priority evaluation module, which generates a mission priority sequence for the flight mission according to the flight mission evaluation rules;

[0009] The charging management module formulates an aircraft charging strategy based on the task priority sequence and the aircraft power information obtained in real time;

[0010] If the emergency task response module receives the emergency task information, it adjusts the flight task priority and the task priority sequence of the aircraft corresponding to the emergency task by comparing the task priority sequence.

[0011] Specifically, the specific process of generating the mission priority sequence of the flight mission includes:

[0012] A1: The mission receiving module obtains flight mission information from the external system and transmits the obtained flight mission information to the mission priority assessment module; the flight mission information includes mission type, mission objective, and mission time requirement;

[0013] A2: The mission priority assessment module assesses each flight mission according to preset flight mission assessment rules; the flight mission assessment rules include the urgency, importance and time requirement of the mission;

[0014] A3: Based on the evaluation results, a priority score P is assigned to each flight mission using the priority score calculation formula. The priority score calculation formula is achieved by taking a weighted sum of the mission's urgency, mission importance, and mission time requirement.

[0015] A4: Sort all flight missions according to their priority scores to generate a mission priority sequence.

[0016] Specifically, the charging management module formulates an aircraft charging strategy based on the mission priority sequence and the aircraft power information obtained in real time, including:

[0017] B1: The charging management module obtains the aircraft's power information in real time and dynamically compares the aircraft's current power level with the power requirements of the tasks in the mission priority sequence. At the same time, a dynamic power demand adjustment mechanism is introduced. If the environment is not a single mission, the system automatically adjusts the calculated power requirements of the task to generate a power comparison result.

[0018] B2: Based on the battery comparison results, select aircraft whose current battery level is lower than the required battery level for the mission. Based on the mission priority sequence and the aircraft's mission execution time window, determine whether the aircraft should perform a charging action.

[0019] If the aircraft's mission execution time window is If it is within, it is marked as emergency charging, where The value is 30 minutes;

[0020] If the aircraft's mission execution time window is If the charge is within the range of 1000, it is marked as normal charging, in which, The value is 120 minutes.

[0021] Specifically, the charging management module formulates an aircraft charging strategy based on the mission priority sequence and the aircraft power information obtained in real time, and further includes:

[0022] B3: Compile the charging priority information of the aircraft to be charged and generate a charging demand list. Based on the charging demand list and the task priority sequence, a charging sequence is determined. The aircraft charging strategy is formulated using a charging time allocation strategy, taking into account the aircraft's power shortage and charging rate. The aircraft charging strategy includes the charging sequence, charging voltage, and charging time.

[0023] B4: The charging device charges the aircraft in sequence according to the aircraft's charging strategy and within a preset charging voltage safety threshold range. The charging voltage safety threshold is 50% of the total voltage.

[0024] B5: Real-time monitoring of charging voltage, current, and temperature. If any abnormality occurs during charging, the system will suspend charging and issue an alarm.

[0025] B6: After charging is completed, the system updates the aircraft's power information. If the aircraft's power level meets the mission requirements, the system marks it as executable.

[0026] Specifically, the specific steps of B3 include:

[0027] B3.1: Based on the power comparison results, select the aircraft to be charged. Based on the mission priority sequence, assign a charging priority to each aircraft to be charged, and generate a charging demand list. The charging demand list includes the aircraft number, current power level, mission power requirement, power gap, and charging priority.

[0028] B3.2: Sort the charging priorities in the charging demand list from high to low to determine the charging order;

[0029] If at least two aircraft have the same charging priority, they will be re-sorted based on the urgency of the mission execution time window;

[0030] B3.3: Calculate the difference between the aircraft's current power and the mission's power requirements to determine the power gap.

[0031] B3.4: Based on the power gap and the charging rate, calculate the charging time by calculating the ratio;

[0032] B3.5: Introduce charging time allocation strategy;

[0033] If the number of charging ports on the charging device is less than the number of aircraft performing charging operations, a dynamic programming algorithm is used to dynamically allocate charging tasks and charging devices.

[0034] If the number of charging ports on the charging device is greater than or equal to the number of aircraft being charged, the parallel charging mechanism is used to charge the aircraft according to the charging priority.

[0035] B3.6: Generate an aircraft charging strategy based on the charging sequence, charging time, and charging device allocation results.

[0036] Specifically, if the emergency task response module receives the emergency task information, adjusting the flight task priority and task priority sequence of the aircraft corresponding to the emergency task by comparing the task priority sequence includes:

[0037] C1: The burst task response module receives the burst task information, pre-processes the burst task information, obtains the pre-processed burst task information, and transmits the pre-processed burst task information to the task priority evaluation module;

[0038] C2: The mission priority assessment module evaluates the priority of the emergency mission information according to the flight mission assessment rules, generates the emergency mission priority, and compares the emergency mission priority with the mission priority in the current mission priority sequence;

[0039] C3: If the priority of the burst task is higher than the priority of the task corresponding to the aircraft waiting to charge or perform a task, the flight task priority of the aircraft corresponding to the burst task is adjusted, and a queue-jumping mechanism is introduced to insert the burst task to the front of the task priority sequence, giving it priority execution;

[0040] C4: The charging management module dynamically updates the aircraft charging strategy based on the adjusted mission priority sequence, reallocates charging resources, and dynamically adjusts the execution order of the original flight missions.

[0041] Specifically, if the emergency task response module receives the emergency task information, adjusting the flight task priority and task priority sequence of the aircraft corresponding to the emergency task by comparing the task priority sequence, further comprising:

[0042] C5: The status monitoring module monitors the status of all aircraft in real time and transmits the monitored status data to the mission priority assessment module and the charging management module;

[0043] C6: The task priority evaluation module dynamically adjusts the task priority sequence based on real-time status data;

[0044] C7: The charging management module dynamically optimizes the aircraft charging strategy based on the dynamically adjusted mission priority sequence and real-time power information;

[0045] C8: The charging equipment charges the aircraft in priority order based on the optimized aircraft charging strategy.

[0046] Specifically, the emergency task information includes task type, task target, and task time requirement; the pre-processed emergency task information includes a emergency task feature vector generated using a task feature extraction algorithm and extracted emergency task urgency and task complexity parameters.

[0047] Specifically, the process of dynamically adjusting the task priority sequence includes:

[0048] If the current battery level of the aircraft is lower than the battery level required for the mission, its mission priority is increased;

[0049] If the aircraft's mission execution progress is delayed, its mission priority is adjusted.

[0050] Compared with the prior art, the present invention has the following beneficial effects:

[0051] 1. The present invention proposes a high-efficiency management and distribution system for low-altitude aircraft, and optimizes and improves the architecture, operating steps and processes. The system has the advantages of simple processes, low investment and operating costs, and low production costs.

[0052] 2. The present invention proposes a high-efficiency management and allocation system for low-altitude aircraft. Through modules such as mission reception and priority assessment, it accurately determines the priority of flight missions, rationally plans charging strategies based on power information and mission priorities, and ensures that aircraft can efficiently perform missions when they have sufficient power. At the same time, a preset charging voltage safety threshold ensures that the aircraft's charging process is safe and reliable, avoiding safety hazards caused by overvoltage charging.

[0053] 3. The present invention proposes a high-efficiency management and allocation system for low-altitude aircraft, which has dynamic adaptability and real-time monitoring optimization mechanism. In the face of emergency tasks, it can quickly evaluate their priorities and adjust the task sequence, so that aircraft resources are prioritized for important tasks, ensuring that emergency tasks are completed efficiently; the status monitoring module provides real-time feedback on the aircraft status, prompting dynamic adjustment of task priorities and charging strategies, further enhancing the flexibility and adaptability of the system, thereby improving the overall utilization efficiency of the aircraft and the quality of mission execution. BRIEF DESCRIPTION OF THE DRAWINGS

[0054] Figure 1 This is an architecture diagram of a high-efficiency management and allocation system for low-altitude aircraft according to the present invention;

[0055] Figure 2 This is a principle flow chart of a high-efficiency management and distribution system for low-altitude aircraft according to the present invention;

[0056] Figure 3 A flow chart is provided for generating a task priority sequence of flight tasks for a high-efficiency management and allocation system for low-altitude aircraft according to the present invention. DETAILED DESCRIPTION

[0057] Example 1

[0058] See also Figure 1 and Figure 2 The present invention provides an embodiment of a high-efficiency management and distribution system for low-altitude aircraft, comprising the following steps:

[0059] Task receiving module, task priority assessment module, charging management module, emergency task response module, status monitoring module, charging equipment module, task execution module;

[0060] The mission receiving module is used to obtain the flight mission information of all aircraft and transmit the flight mission information to subsequent modules for processing;

[0061] The mission priority evaluation module is used to assign a priority to each flight mission according to the preset flight mission evaluation rules, generate a mission priority sequence, and dynamically adjust the priority when sudden missions occur;

[0062] The charging management module is used to monitor the aircraft's power information in real time, formulate charging strategies, and ensure that the charging voltage does not exceed the safety threshold during the charging process;

[0063] The emergency task response module is used to receive emergency task information and transmit it to the task priority evaluation module for priority evaluation and dynamic adjustment;

[0064] The status monitoring module is used to monitor the status of all aircraft in real time and transmit the monitored status data to related modules for dynamic adjustment and optimization;

[0065] The charging device module is used to provide charging services for the aircraft according to the charging strategy formulated by the charging management module and ensure that the charging voltage is within a safe range;

[0066] The mission execution module is used to schedule aircraft to perform missions according to the mission priority sequence and dynamically adjust the mission execution order when sudden missions occur.

[0067] The task receiving module includes: a task acquiring unit and a task transmitting unit;

[0068] A mission acquisition unit, used to obtain flight mission information from an external system or user input;

[0069] The mission transmission unit is used to transmit the acquired flight mission information to the mission priority assessment module.

[0070] The task priority evaluation module includes: a task evaluation unit, a priority sequence generation unit, a burst task evaluation unit, and a dynamic adjustment unit;

[0071] A mission evaluation unit, configured to assign a priority to each flight mission according to flight mission evaluation rules; the flight mission evaluation rules include the urgency, importance, and time requirements of the mission;

[0072] A priority sequence generating unit, used to sort the priorities of the evaluated tasks and generate a task priority sequence;

[0073] The emergency task evaluation unit is used to, when receiving the emergency task information, perform priority evaluation on the emergency task information according to the flight task evaluation rules and generate the emergency task priority;

[0074] The dynamic adjustment unit is used to dynamically adjust the task priority sequence according to the burst task priority or real-time status data.

[0075] The charging management module includes: power monitoring unit, charging demand judgment unit, charging strategy formulation unit, charging execution unit, and dynamic optimization unit;

[0076] Power monitoring unit, used to obtain real-time power information of all aircraft;

[0077] A charging demand judgment unit is used to compare the current power level of the aircraft with the power required for the mission, determine whether to perform charging action, and generate a charging demand list;

[0078] A charging strategy formulation unit, used to formulate an aircraft charging strategy based on the mission priority sequence and the charging requirement list;

[0079] The charging execution unit is used to control the charging device to charge the aircraft within a preset charging voltage safety threshold range according to the aircraft charging strategy.

[0080] The dynamic optimization unit is used to dynamically optimize the charging strategy according to the adjusted task priority sequence and real-time power information.

[0081] The burst task response module includes: a burst task receiving unit and a burst task transmitting unit;

[0082] A burst task receiving unit, used to obtain burst task information from an external system or user input;

[0083] The burst task transmission unit is used to transmit the burst task information to the task priority evaluation module.

[0084] The status monitoring module includes: a status data acquisition unit and a status data transmission unit;

[0085] Status data acquisition unit, used to collect real-time status data of the aircraft, such as power level, location, and mission execution progress;

[0086] The status data transmission unit is used to transmit the collected status data to the task priority evaluation module and the charging management module.

[0087] It should be noted that the task receiving module transmits the flight mission information to the task priority evaluation module to generate a task priority sequence; the charging management module formulates a charging strategy and controls the charging equipment module based on the task priority sequence and power information; the emergency task response module transmits the emergency task information to the task priority evaluation module to trigger dynamic adjustment; the status monitoring module collects the aircraft status data in real time and transmits it to the task priority evaluation module and the charging management module for dynamic optimization; the task execution module schedules the aircraft to perform tasks according to the task priority sequence, and makes dynamic adjustments when necessary.

[0088] Specifically, the overall implementation process of a high-efficiency management and allocation system for low-altitude aircraft includes:

[0089] The mission receiving module obtains the flight mission information of the aircraft and transmits the flight mission information to the mission priority evaluation module. The mission priority evaluation module assigns a priority to each flight mission according to the flight mission evaluation rules to form a mission priority sequence;

[0090] The charging management module obtains the aircraft's power information in real time and compares it with the power requirements of the missions in the mission priority sequence. If the aircraft's power level is lower than the mission's required power level, the charging management module determines whether the aircraft needs to be charged immediately based on the mission priority sequence and generates a charging demand list.

[0091] The charging management module formulates the aircraft charging strategy based on the charging demand list and task priority sequence. The charging equipment charges the aircraft in sequence according to the aircraft charging strategy and within the preset charging voltage safety threshold range;

[0092] If the emergency task response module receives the emergency task information, it will transmit the emergency task information to the task priority evaluation module. The task priority evaluation module will evaluate the priority of the emergency task according to the flight task evaluation rules and generate the emergency task priority. If the priority of the emergency task is higher than the task priority corresponding to the aircraft waiting in line for charging or performing tasks, the flight task priority of the aircraft corresponding to the emergency task will be adjusted to allow it to jump the queue and enter the charging process or perform tasks first.

[0093] The charging management module dynamically updates the aircraft charging strategy based on the adjusted mission priority sequence, reallocates charging resources, and dynamically adjusts the execution order of the original flight missions;

[0094] The status monitoring module monitors the status of all aircraft in real time and transmits the monitored status data to the mission priority assessment module and the charging management module;

[0095] The task priority evaluation module dynamically adjusts the task priority sequence based on real-time status data;

[0096] The charging management module dynamically optimizes the aircraft charging strategy based on the dynamically adjusted mission priority sequence and real-time power information.

[0097] Example 2

[0098] See also Figure 3 The specific process of generating the mission priority sequence of the flight mission in this embodiment includes:

[0099] A1: The mission receiving module obtains flight mission information from the external system and transmits the obtained flight mission information to the mission priority assessment module; the flight mission information includes mission type, mission objective, and mission time requirement;

[0100] A2: The mission priority assessment module evaluates each flight mission according to preset flight mission assessment rules; the flight mission assessment rules include three dimensions: urgency, importance, and time requirement of the mission;

[0101] Furthermore, the specific process of evaluating each flight mission includes:

[0102] (1) Obtain flight mission information and define three evaluation dimensions based on the preset flight mission evaluation rules:

[0103] Urgency: The urgency with which the task needs to be executed, ranging from 1 to 5, with 5 being the most urgent;

[0104] Importance: The degree to which the task affects the overall task goal, with a value range of 1-5, with 5 being the most important;

[0105] Time requirement: The time limit for completing the task, ranging from 1 to 5, with 5 being the most urgent;

[0106] (2) Assign a weight coefficient to each evaluation dimension, and the cumulative sum of the weight coefficients is 1.

[0107] A3: Based on the evaluation results, a priority score P is assigned to each flight mission using the priority score calculation formula. The priority score calculation formula is achieved by taking a weighted sum of the mission's urgency, mission importance, and mission time requirement. The specific formula is: ,in, Indicates the urgency of the task. Indicates the importance of the task, Indicates the time requirement of the task, and satisfies , 、 、 The weight coefficients representing the urgency, importance and time requirement of the task respectively;

[0108] A4: Sort all flight missions according to their priority scores to generate a mission priority sequence.

[0109] Based on the mission priority sequence and the real-time aircraft power information, the charging management module formulates the aircraft charging strategy, including:

[0110] B1: The charging management module obtains the aircraft's power information in real time and dynamically compares the aircraft's current power level with the power requirements of the missions in the mission priority sequence. At the same time, a dynamic power demand adjustment mechanism is introduced. If the power consumption is affected by external factors such as wind speed and temperature in a non-single mission environment, the system automatically adjusts the calculated power requirements of the mission and generates a power comparison result.

[0111] Furthermore, the specific steps of B1 include:

[0112] (1) The charging management module obtains the power information of all aircraft in real time through wireless communication technology, including the current power percentage and battery health status;

[0113] (2) Obtain the power required for each flight mission from the mission priority sequence ;

[0114] (3) A dynamic power demand adjustment mechanism is introduced to adjust the calculated power required for the task according to the complexity of the task environment. The adjustment formula is: ,in, represents the power required for the adjusted task, k represents the environmental complexity impact coefficient, and C represents the environmental complexity score. The environmental complexity score needs to be determined by technicians in this field through a large number of experiments or pre-set based on expert experience.

[0115] (4) The current battery level of the aircraft The power required for the task after adjustment Compare, if , then mark the aircraft to perform charging action;

[0116] (5) Organize and generate power comparison results, including aircraft number, current power, adjusted mission power requirements, power gap and other information.

[0117] B2: Based on the battery comparison results, select aircraft whose current battery level is lower than the required battery level for the mission. Based on the mission priority sequence and the aircraft's mission execution time window, determine whether the aircraft should perform a charging action.

[0118] If the aircraft's mission execution time window is If it is within, it is marked as emergency charging, where The value is 30 minutes;

[0119] If the aircraft's mission execution time window is If the charge time is within 10 seconds, it is marked as normal charging, in which, The value is 120 minutes;

[0120] B3: Compile the charging priority information of the aircraft to be charged and generate a charging demand list. Based on the charging demand list and the task priority sequence, a charging sequence is determined. The aircraft charging strategy is formulated using a charging time allocation strategy, taking into account the aircraft's power shortage and charging rate. The aircraft charging strategy includes the charging sequence, charging voltage, and charging time.

[0121] B4: The charging device charges the aircraft in sequence according to the aircraft's charging strategy and within a preset charging voltage safety threshold range. The charging voltage safety threshold is 50% of the total voltage.

[0122] B5: Real-time monitoring of charging voltage, current, and temperature. If any abnormality occurs during charging, the system will immediately suspend charging and issue an alarm.

[0123] Among them, abnormal conditions include battery overheating and communication interruption.

[0124] B6: After charging is completed, the system updates the aircraft's power information. If the aircraft's power level meets the mission requirements, the system marks it as executable.

[0125] The specific steps of B3 include:

[0126] B3.1: Based on the power comparison results, select the aircraft to be charged. Based on the mission priority sequence, assign a charging priority to each aircraft to be charged, and generate a charging demand list. The charging demand list includes the aircraft number, current power level, mission power requirement, power gap, and charging priority.

[0127] B3.2: Sort the charging priorities in the charging demand list from high to low to determine the charging order;

[0128] If at least two aircraft have the same charging priority, they will be re-sorted based on the urgency of the mission execution time window;

[0129] B3.3: Calculate the power gap by calculating the difference between the aircraft's current power and the power required for the mission.

[0130] B3.4: Based on the power gap and the charging rate, calculate the charging time by calculating the ratio;

[0131] B3.5: Introduce charging time allocation strategy;

[0132] If the number of charging ports on the charging device is less than the number of aircraft performing charging operations, a dynamic programming algorithm is used to dynamically allocate charging tasks and charging devices.

[0133] Furthermore, the specific process of dynamic programming includes:

[0134] (1) Model the charging task allocation problem as a dynamic programming problem;

[0135] (2) Define the state ,in, Indicates the allocation of the first i charging tasks and the first j charging devices, i represents the index of the charging task, and j represents the index of the charging device;

[0136] (3) Define decision variables ,in, Indicates whether the i-th charging task is assigned to the j-th charging device, and satisfies: when task i is assigned to device j, ,otherwise, ;

[0137] (4) Define the objective function, where the objective function is to minimize the total completion time of all charging tasks;

[0138] (5) Set constraints, including that each charging task can only be assigned to one charging device and the total charging time of each charging device does not exceed its maximum available time;

[0139] (6) The dynamic programming transfer equation is used to solve the above dynamic programming problem and obtain the optimal charging task allocation plan. The dynamic programming transfer equation is the existing technical content in this field and is not the inventive solution of this application, so it will not be described in detail here.

[0140] If the number of charging ports on the charging device is greater than or equal to the number of aircraft being charged, the parallel charging mechanism is used to charge the aircraft according to the charging priority.

[0141] B3.6: Generate an aircraft charging strategy based on the charging sequence, charging time, and charging device allocation results.

[0142] If the emergency task response module receives the emergency task information, the flight task priority and the task priority sequence of the aircraft corresponding to the emergency task are adjusted by comparing the task priority sequence, including:

[0143] C1: The burst task response module receives the burst task information, pre-processes the burst task information, obtains the pre-processed burst task information, and transmits the pre-processed burst task information to the task priority evaluation module;

[0144] The sudden task information described in C1 includes task type, task objective, and task time requirement; the preprocessed sudden task information includes a sudden task feature vector generated using a task feature extraction algorithm and extracted sudden task urgency and task complexity parameters, wherein the task feature extraction algorithm adopts the principal component analysis method, and the principal component analysis method is the existing technology content in this field and is not the inventive solution of this application, and will not be elaborated here.

[0145] C2: The mission priority assessment module evaluates the priority of the emergency mission information according to the flight mission assessment rules, generates the emergency mission priority, and compares the emergency mission priority with the mission priority in the current mission priority sequence;

[0146] C3: If the priority of the burst task is higher than the priority of the task corresponding to the aircraft waiting to charge or perform a task, the flight task priority of the aircraft corresponding to the burst task is adjusted, and a queue-jumping mechanism is introduced to insert the burst task to the front of the task priority sequence, giving it priority execution;

[0147] C4: The charging management module dynamically updates the aircraft charging strategy based on the adjusted mission priority sequence, reallocates charging resources, and dynamically adjusts the execution order of the original flight missions;

[0148] C5: The status monitoring module monitors the status of all aircraft in real time and transmits the monitored status data to the mission priority assessment module and the charging management module;

[0149] C6: The task priority evaluation module dynamically adjusts the task priority sequence based on real-time status data;

[0150] The process of dynamically adjusting the task priority sequence in C6 includes:

[0151] If the aircraft's battery level is lower than the mission's required power level, its mission priority is increased;

[0152] If the aircraft's mission execution progress is delayed, its mission priority is adjusted.

[0153] C7: The charging management module dynamically optimizes the aircraft charging strategy based on the dynamically adjusted mission priority sequence and real-time power information;

[0154] C8: The charging equipment charges the aircraft in priority order based on the optimized aircraft charging strategy.

[0155] The embodiments of the present invention are described above in conjunction with the accompanying drawings, but the present invention is not limited to the above-mentioned specific embodiments. The above-mentioned specific embodiments are merely illustrative and not restrictive. Under the guidance of the present invention, ordinary technicians in this field can also change, modify, replace and modify the above-mentioned embodiments without departing from the purpose and scope of protection of the present invention. These are all protected by the present invention.

Claims

1. A high-efficiency management and distribution system for low-altitude aircraft, characterized in that: include: Task receiving module, task priority assessment module, charging management module, emergency task response module; The mission receiving module obtains the flight mission information of the aircraft and transmits it to the mission priority evaluation module, which generates a mission priority sequence for the flight mission according to the flight mission evaluation rules; The charging management module formulates an aircraft charging strategy based on the task priority sequence and the aircraft power information obtained in real time; If the emergency task response module receives the emergency task information, it adjusts the flight task priority and the task priority sequence of the aircraft corresponding to the emergency task by comparing the task priority sequence; The charging management module formulates an aircraft charging strategy based on the mission priority sequence and the aircraft power information obtained in real time, including: B1: The charging management module obtains the aircraft's power information in real time and dynamically compares the aircraft's current power level with the power requirements of the tasks in the mission priority sequence. At the same time, a dynamic power demand adjustment mechanism is introduced. If the environment is not a single mission, the system automatically adjusts the calculated power requirements of the task to generate a power comparison result. B2: Based on the battery comparison results, select aircraft whose current battery level is lower than the required battery level for the mission. Based on the mission priority sequence and the aircraft's mission execution time window, determine whether the aircraft should perform a charging action. If the aircraft's mission execution time window is If it is within, it is marked as emergency charging, where The value is 30 minutes; If the aircraft's mission execution time window is If the charge is within the range of 1000, it is marked as normal charging, in which, The value is 120 minutes; The charging management module formulates an aircraft charging strategy based on the mission priority sequence and the aircraft power information obtained in real time, further comprising: B3: Compile the charging priority information of the aircraft to be charged and generate a charging demand list. Based on the charging demand list and the task priority sequence, a charging sequence is determined. The aircraft charging strategy is formulated using a charging time allocation strategy, taking into account the aircraft's power shortage and charging rate. The aircraft charging strategy includes the charging sequence, charging voltage, and charging time. B4: The charging device charges the aircraft in sequence according to the aircraft's charging strategy and within the preset charging voltage safety threshold range. B5: Real-time monitoring of charging voltage, current, and temperature. If any abnormality occurs during charging, the system will suspend charging and issue an alarm. B6: After charging is completed, the system updates the aircraft's power information. If the aircraft's power level meets the mission requirements, the system marks it as mission-ready. The specific steps of B1 include: B1.1: The charging management module obtains the power information of all aircraft in real time through wireless communication technology, including the current power percentage and battery health status; B1.2: Obtain the power required for each flight mission from the mission priority sequence ; B1.3: Introduce a dynamic power demand adjustment mechanism to adjust the calculated power required for the task based on the complexity of the task environment. The adjustment formula is: ,in, represents the power required for the task after adjustment, k represents the environmental complexity impact coefficient, and C represents the environmental complexity score; B1.4: The current battery level of the aircraft The power required for the adjusted task Compare, if , then mark the aircraft to perform charging action; B1.5: Organize the comparison results of generated electricity; The specific steps of B3 include: B3.1: Based on the power comparison results, select the aircraft to be charged. Based on the mission priority sequence, assign a charging priority to each aircraft to be charged, and generate a charging demand list. The charging demand list includes the aircraft number, current power level, mission power requirement, power gap, and charging priority. B3.2: Sort the charging priorities in the charging demand list from high to low to determine the charging order; If at least two aircraft have the same charging priority, they will be re-sorted based on the urgency of the mission execution time window; B3.3: Calculate the difference between the aircraft's current power and the mission's power requirements to determine the power gap. B3.4: Based on the power gap and the charging rate, calculate the charging time by calculating the ratio; B3.5: Introduce charging time allocation strategy; If the number of charging ports on the charging device is less than the number of aircraft performing charging operations, a dynamic programming algorithm is used to dynamically allocate charging tasks and charging devices. If the number of charging ports on the charging device is greater than or equal to the number of aircraft being charged, the parallel charging mechanism is used to charge the aircraft according to the charging priority. B3.6: Generate an aircraft charging strategy based on the charging sequence, charging time, and charging device allocation results.

2. A high-efficiency management and distribution system for low-altitude aircraft according to claim 1, characterized in that: The specific process of generating the mission priority sequence of the flight mission includes: A1: The mission receiving module obtains flight mission information from the external system and transmits the obtained flight mission information to the mission priority assessment module; the flight mission information includes mission type, mission objective, and mission time requirement; A2: The mission priority assessment module assesses each flight mission according to preset flight mission assessment rules; the flight mission assessment rules include the urgency, importance and time requirement of the mission; A3: Based on the evaluation results, a priority score P is assigned to each flight mission using the priority score calculation formula. The priority score calculation formula is achieved by taking a weighted sum of the mission's urgency, mission importance, and mission time requirement. A4: Sort all flight missions according to their priority scores to generate a mission priority sequence.

3. A high-efficiency management and distribution system for low-altitude aircraft according to claim 1, characterized in that: If the emergency task response module receives the emergency task information, adjusting the flight task priority and the task priority sequence of the aircraft corresponding to the emergency task by comparing the task priority sequence includes: C1: The burst task response module receives the burst task information, pre-processes the burst task information, obtains the pre-processed burst task information, and transmits the pre-processed burst task information to the task priority evaluation module; C2: The mission priority assessment module evaluates the priority of the emergency mission information according to the flight mission assessment rules, generates the emergency mission priority, and compares the emergency mission priority with the mission priority in the current mission priority sequence; C3: If the priority of the burst task is higher than the priority of the task corresponding to the aircraft waiting to charge or perform a task, the flight task priority of the aircraft corresponding to the burst task is adjusted, and a queue-jumping mechanism is introduced to insert the burst task to the front of the task priority sequence, giving it priority execution; C4: The charging management module dynamically updates the aircraft charging strategy based on the adjusted mission priority sequence, reallocates charging resources, and dynamically adjusts the execution order of the original flight missions.

4. A high-efficiency management and distribution system for low-altitude aircraft as claimed in claim 3, characterized in that: If the emergency task response module receives the emergency task information, adjusting the flight task priority and the task priority sequence of the aircraft corresponding to the emergency task by comparing the task priority sequence, further comprising: C5: The status monitoring module monitors the status of all aircraft in real time and transmits the monitored status data to the mission priority assessment module and the charging management module; C6: The task priority evaluation module dynamically adjusts the task priority sequence based on real-time status data; C7: The charging management module dynamically optimizes the aircraft charging strategy based on the dynamically adjusted mission priority sequence and real-time power information; C8: The charging equipment charges the aircraft in priority order based on the optimized aircraft charging strategy.

5. A high-efficiency management and distribution system for low-altitude aircraft according to claim 4, characterized in that: The sudden task information includes task type, task target, and task time requirement; the pre-processed sudden task information includes a sudden task feature vector generated using a task feature extraction algorithm and extracted sudden task urgency and task complexity parameters.

6. A high-efficiency management and distribution system for low-altitude aircraft according to claim 5, characterized in that: The process of dynamically adjusting the task priority sequence includes: If the current battery level of the aircraft is lower than the battery level required for the mission, its mission priority is increased; If the aircraft's mission execution progress is delayed, its mission priority is adjusted.

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