A warehouse door dynamic control method, device and computer readable storage medium

Abstract

The present invention discloses a method, device, and computer-readable storage medium for dynamic control of cargo hold doors, wherein the method comprises: when an aircraft takes off with a cargo hold, obtaining the stored power of the four side doors and one bottom door of the cargo hold, wherein the four side doors and the bottom door all contain battery modules; when setting the bottom door to pick up items, determining that the power supply priority of the battery modules contained in the bottom doors is higher than the power supply priority of the battery modules contained in the four side doors; and when setting the side door to pick up items, determining that the power supply priority of the battery modules contained in the four side doors is higher than the power supply priority of the battery modules contained in the bottom door. The present invention implements a dynamic control scheme for cargo hold doors and door batteries, so that the cargo hold can adaptively adjust the door power supply mode according to the open doors, while providing additional battery life for the aircraft, and can also flexibly and efficiently transfer and charge the batteries of the cargo hold cargo.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of unmanned aerial vehicles, in particular to a cargo compartment door dynamic control method, device and computer readable storage medium. BACKGROUND

[0002] In the prior art, with the continuous development of manned aircraft technology, unmanned aerial vehicle logistics has begun to be popularized and promoted. In particular, unmanned aerial vehicle logistics needs to consider the timeliness of logistics operations, both to ensure the cargo carrying capacity and to ensure the endurance. However, in the traditional unmanned aerial vehicle logistics operation, the battery and the carried cargo compartment of the unmanned aerial vehicle need to be replaced respectively, which is relatively cumbersome and time-consuming, and at the same time, the battery and the cargo compartment arranged in the unmanned aerial vehicle body also occupy a lot of space inside the unmanned aerial vehicle.

[0003] Therefore, how to optimize the timeliness in the process of unmanned aerial vehicle logistics operation, on the basis of improving the cargo carrying space, further improve the endurance, has become a technical problem to be solved at present. SUMMARY

[0004] In order to solve the above technical defects in the prior art, the present application provides a cargo compartment door dynamic control method, which comprises:

[0005] When the aircraft carrying the cargo compartment takes off, the storage power of the four side compartment doors and one bottom compartment door of the cargo compartment is obtained, wherein the four side compartment doors and the bottom compartment door each contain a battery module;

[0006] When the estimated consumption power of the current flight exceeds the storage power of a single side compartment door or bottom compartment door, the target storage cabinet setting of the cargo compartment opening surface is obtained;

[0007] When the bottom door pickup is set, it is determined that the power supply priority of the battery module contained in the bottom compartment door is higher than that of the battery module contained in the four side compartment doors, and when the side door pickup is set, it is determined that the power supply priority of the battery module contained in the four side compartment doors is higher than that of the battery module contained in the bottom compartment door;

[0008] When the aircraft carrying the cargo compartment lands, if it is a bottom door pickup, the bottom compartment door supports the goods into the target storage cabinet, and if it is a side door pickup, the side compartment door with the lowest power is laid down and supports the goods into the target storage cabinet.

[0009] Optionally, when the aircraft carrying the cargo compartment takes off, the storage power of the four side compartment doors and one bottom compartment door of the cargo compartment is obtained, wherein the four side compartment doors and the bottom compartment door each contain a battery module, and the previous step comprises:

[0010] Detecting the current delivery compartment door of the aircraft;

[0011] In the case of bottom door drop, the goods are transferred into the cargo compartment by the bottom door support carrying the full battery module, and the cargo compartment is closed by the bottom door. In the case of side door drop, the goods are transferred into the cargo compartment by the side door support carrying the full battery module, and the cargo compartment is closed by the side door by being erected.

[0012] Optionally, the method further comprises:

[0013] Obtaining the minimum power storage door among the four side doors and the bottom door;

[0014] Detecting whether the minimum power storage door meets the estimated power consumption.

[0015] Optionally, the method further comprises:

[0016] In the case of the minimum power storage door being a side door and the minimum power storage door not meeting the estimated power consumption, setting the power supply priority of the battery modules contained in the minimum power storage side door, the other three side doors and the bottom door from high to low in the case of side door pickup.

[0017] In the case of the minimum power storage door being a side door and the minimum power storage door not meeting the estimated power consumption, setting the power supply priority of the battery modules contained in the minimum power storage side door, the bottom door and the other three side doors from high to low in the case of bottom door pickup.

[0018] Optionally, the method further comprises:

[0019] In the case of the minimum power storage door being a bottom door and the minimum power storage door not meeting the estimated power consumption, determining that the power supply priority of the battery modules contained in the four side doors is higher than the power supply priority of the battery modules contained in the bottom door in the case of side door pickup.

[0020] In the case of the minimum power storage door being a bottom door and the minimum power storage door not meeting the estimated power consumption, determining that the power supply priority of the battery modules contained in the bottom door is higher than the power supply priority of the battery modules contained in the four side doors in the case of bottom door pickup.

[0021] The application further provides a cargo compartment door dynamic control device, which comprises a memory, a processor and a computer program stored in the memory and executable on the processor, and the computer program is executed by the processor to realize:

[0022] When the aircraft carrying the cargo compartment takes off, obtaining the storage power of the four side doors and the bottom door of the cargo compartment, wherein the four side doors and the bottom door all contain battery modules.

[0023] when the estimated consumption power of the current flight exceeds the storage power of the side door or the bottom door, obtaining a target storage compartment of the current flight set by the warehouse opening surface;

[0024] when the bottom door is set for picking, the power supply priority of the battery module contained in the bottom door is higher than the power supply priority of the battery module contained in the four side doors, and when the side door is set for picking, the power supply priority of the battery module contained in the four side doors is higher than the power supply priority of the battery module contained in the bottom door;

[0025] when the aircraft carrying the cargo compartment lands, if it is bottom door picking, the goods are transferred into the target storage compartment by the bottom door, and if it is side door picking, the lowest power side door is laid down and the goods are transferred into the target storage compartment.

[0026] Optionally, the computer program is executed by the processor to realize:

[0027] detecting the current delivery door of the aircraft;

[0028] when it is determined to be a bottom door delivery, the goods are transferred into the cargo compartment by the bottom door carrying the full power battery module, and the cargo compartment is closed by the bottom door, and when it is determined to be a side door delivery, the goods are transferred into the cargo compartment by the side door carrying the full power battery module, and the cargo compartment is closed by the side door by standing up.

[0029] Optionally, the computer program is executed by the processor to realize:

[0030] obtaining the minimum power storage door among the four side doors and the bottom door;

[0031] detecting whether the minimum power storage door meets the estimated consumption power.

[0032] Optionally, the computer program is executed by the processor to realize:

[0033] when the minimum power storage door is a side door and the minimum power storage door does not meet the estimated consumption power, setting the side door picking, and setting the power supply priority of the battery module contained in the minimum power storage side door, the other three side doors and the bottom door from high to low;

[0034] when the minimum power storage door is a side door and the minimum power storage door does not meet the estimated consumption power, setting the bottom door picking, and setting the power supply priority of the battery module contained in the minimum power storage side door, the bottom door and the other three side doors from high to low;

[0035] In the case that the minimum storage power bin door is a bottom bin door and the minimum storage power bin door does not meet the estimated power consumption, when the side door pick-up is set, the power supply priority of the battery modules contained in the four side bin doors is higher than the power supply priority of the battery modules contained in the bottom bin door.

[0036] In the case that the minimum storage power bin door is a bottom bin door and the minimum storage power bin door does not meet the estimated power consumption, when the bottom door pick-up is set, the power supply priority of the battery modules contained in the bottom bin door is higher than the power supply priority of the battery modules contained in the four side bin doors.

[0037] The application further provides a computer readable storage medium, which stores a warehouse bin door dynamic control program. When the warehouse bin door dynamic control program is executed by a processor, the steps of the warehouse bin door dynamic control method according to any one of the preceding embodiments are implemented.

[0038] The warehouse bin door dynamic control method, device and computer readable storage medium according to the application are characterized in that: when the aircraft carrying the warehouse takes off, the storage power of the four side bin doors and one bottom bin door of the warehouse is obtained, wherein the four side bin doors and the bottom bin door each contain battery modules; when the estimated power consumption of the current flight exceeds the storage power of a single side bin door or bottom bin door, the target storage cabinet set by the warehouse opening surface of the current flight is obtained; when the bottom door pick-up is set, the power supply priority of the battery modules contained in the bottom bin door is higher than the power supply priority of the battery modules contained in the four side bin doors; when the side door pick-up is set, the power supply priority of the battery modules contained in the four side bin doors is higher than the power supply priority of the battery modules contained in the bottom bin door; when the aircraft carrying the warehouse lands, if the bottom door pick-up, the goods are transferred into the target storage cabinet by the bottom bin door; if the side door pick-up, the side bin door with the lowest power is laid down and the goods are transferred into the target storage cabinet. The warehouse bin door and bin door battery dynamic control scheme is realized, so that the warehouse can adaptively allocate the power supply of the bin door according to the opened bin door, and the additional endurance power of the aircraft can be used to flexibly and efficiently transfer and charge the goods in the warehouse. BRIEF DESCRIPTION OF DRAWINGS

[0039] The application will be further described below with reference to the accompanying drawings and embodiments. In the drawings:

[0040] Figure 1 is the first flowchart of the warehouse bin door dynamic control method according to the application;

[0041] Figure 2 is the second flowchart of the warehouse bin door dynamic control method according to the application;

[0042] Figure 3 is the third flowchart of the warehouse bin door dynamic control method according to the application;

[0043] Figure 4 is the fourth flow chart of the warehouse door dynamic control method of the present application;

[0044] Figure 5 is the fifth flow chart of the warehouse door dynamic control method of the present application. DETAILED DESCRIPTION

[0045] It should be understood that the specific embodiments described herein are merely exemplary and do not limit the application.

[0046] In the following description, the suffixes used for elements such as "module", "part", or "unit" are used only for convenience of explanation of the present application, and have no specific meaning by themselves. Therefore, "module", "part", or "unit" can be mixedly used.

[0047] Figure 1 is the first flow chart of the warehouse door dynamic control method of the present application. The embodiment proposes a warehouse door dynamic control method, which comprises:

[0048] S1, when an aircraft carrying a warehouse takes off, the storage power of four side doors and one bottom door of the warehouse is obtained, wherein the four side doors and the bottom door each contain a battery module;

[0049] S2, when the estimated consumption power of the current flight exceeds the storage power of a single side door or the bottom door, the target storage cabinet setting of the warehouse opening surface of the current flight is obtained;

[0050] S3, when setting the bottom door to pick up, it is determined that the power supply priority of the battery module contained in the bottom door is higher than that of the battery module contained in the four side doors, and when setting the side door to pick up, it is determined that the power supply priority of the battery module contained in the four side doors is higher than that of the battery module contained in the bottom door;

[0051] S4, when the aircraft carrying the warehouse lands, if the bottom door is set to pick up, the bottom door supports the goods into the target storage cabinet, and if the side door is set to pick up, the side door with the lowest power is laid down and supports the goods into the target storage cabinet.

[0052] In the embodiment, the aircraft is a fixed-wing unmanned aerial vehicle or a multi-rotor unmanned aerial vehicle, which can be built-in with one or more cargo compartments, and the cargo compartment is spliced by a plurality of independent battery modules, that is, each battery module can be used as a separate splicing module. For example, a plurality of splicing modules can be spliced into a rectangular body as a cargo compartment for goods. Further, in the embodiment, the cargo compartment is spliced by six independent surfaces, each of which is an independent battery module, or a plurality of independent battery modules are spliced into a surface. Further, in the embodiment, the four side surfaces and the bottom surface of the cargo compartment can independently supply power to the aircraft. Alternatively, in the embodiment, the four side surfaces and the bottom surface of the cargo compartment are used as four side doors and a bottom door of the cargo compartment, respectively. Alternatively, in the embodiment, a power supply module is arranged on the top surface of the cargo compartment, which is electrically connected with the power supply module of the aircraft on one hand, and is electrically connected with the four side doors and the bottom door on the other hand, so that the power of any one of the four side surfaces and the bottom surface can be provided to the aircraft.

[0053] In the embodiment, when the estimated consumption power of the current flight exceeds the storage power of a single side door or bottom door, the target storage cabinet setting of the cargo compartment opening surface of the current flight is obtained. When it is determined that a single surface door cannot meet the required power of the current flight, the decision of the door with priority consumption power is started. Specifically, first, the target storage cabinet setting of the cargo compartment opening surface of the current flight is obtained. For example, when the aircraft lands on the top end of the target storage cabinet, the bottom door is set as the cargo compartment opening surface, and when the aircraft lands on the side of the target storage cabinet, the side door is set as the cargo compartment opening surface. The actual situation of the target storage cabinet can also be considered for corresponding setting. Alternatively, the pickup setting mode of the target storage cabinet is obtained by communicating with the target storage cabinet, or the pickup setting mode of the target storage cabinet is set or queried by communicating with the server.

[0054] In the embodiment, when the bottom door pickup is set, it is determined that the power supply priority of the battery modules included in the bottom door is higher than that of the battery modules included in the four side doors, and when the side door pickup is set, it is determined that the power supply priority of the battery modules included in the four side doors is higher than that of the battery modules included in the bottom door. When the bottom door pickup is set, the aircraft is powered by the battery modules included in the bottom door in priority, and when the side door pickup is set, the aircraft is powered by the battery modules included in the side door in priority. Alternatively, the opening orientation of the target storage cabinet is obtained, and the corresponding cargo compartment opening side door on the aircraft is determined according to the opening orientation. Based on this, when the side door pickup is set, the aircraft is powered by the battery modules included in the corresponding side door of the opening side door in priority.

[0055] In the embodiment, when the aircraft carrying the cargo compartment lands, if the bottom door is used for picking up, the bottom compartment door supports the goods to be transferred into the target storage cabinet, and if the side door is used for picking up, the lowest power side compartment door is laid down and supports the goods to be transferred into the target storage cabinet. In the embodiment, based on the opening direction of the target storage cabinet obtained in the above-mentioned embodiment, the opening side door of the cargo compartment on the aircraft is determined according to the opening direction. When the side door is used for picking up, the side compartment door corresponding to the opening side door is laid down and supports the goods to be transferred into the target storage cabinet.

[0056] The embodiment has the beneficial effect that, when the aircraft carrying the cargo compartment takes off, the storage power of four side compartment doors and one bottom compartment door of the cargo compartment is obtained, wherein the four side compartment doors and the bottom compartment door each include a battery module; when the estimated consumption power of the current flight exceeds the storage power of a single side compartment door or the bottom compartment door, the opening face of the cargo compartment set for the target storage cabinet of the current flight is obtained; when the bottom door is used for picking up, the power supply priority of the battery module included in the bottom compartment door is determined to be higher than that of the battery module included in the four side compartment doors, and when the side door is used for picking up, the power supply priority of the battery module included in the four side compartment doors is determined to be higher than that of the battery module included in the bottom compartment door; when the aircraft carrying the cargo compartment lands, if the bottom door is used for picking up, the bottom compartment door supports the goods to be transferred into the target storage cabinet, and if the side door is used for picking up, the lowest power side compartment door is laid down and supports the goods to be transferred into the target storage cabinet. A dynamic control scheme for the cargo compartment door and the compartment door battery is realized, so that the cargo compartment can adaptively allocate the power supply of the compartment door according to the opening of the compartment door, and the additional endurance power brought by the aircraft can be flexibly and efficiently used for the battery transfer and charging of the goods in the cargo compartment.

[0057] Figure 2 The second flowchart is a dynamic control method for the cargo compartment door of the present application, based on the above-mentioned embodiment, wherein the storage power of four side compartment doors and one bottom compartment door of the cargo compartment is obtained when the aircraft carrying the cargo compartment takes off, wherein the four side compartment doors and the bottom compartment door each include a battery module, and the above-mentioned embodiment includes:

[0058] S01, detecting the current put-down compartment door of the aircraft;

[0059] S02, when it is determined that the bottom door is used for putting down, the bottom compartment door carrying the full-power battery module supports the goods to be transferred into the cargo compartment, and the bottom compartment door closes the cargo compartment; when it is determined that the side door is used for putting down, the side compartment door carrying the full-power battery module supports the goods to be transferred into the cargo compartment, and the side compartment door is then straightened to close the cargo compartment.

[0060] Optionally, in the present embodiment, when it is determined that the bottom door is used for taking out the goods, and it is determined that the estimated power consumption of the current flight of the aircraft is greater than the preset power, the double-layer bottom cargo door carrying the full-power battery module supports the goods into the cargo compartment, and the bottom cargo door at the bottom seals the cargo compartment.

[0061] Optionally, in the present embodiment, when it is determined that the side door is used for taking out the goods, and it is determined that the estimated power consumption of the current flight of the aircraft is greater than the preset power, after the side cargo door carrying the full-power battery module and the bottom cargo door carrying the full-power battery module jointly support the goods into the cargo compartment, the side cargo door is erected to seal the side edge of the cargo compartment, and the bottom cargo door seals the bottom edge of the cargo compartment.

[0062] Figure 3 FIG. 3 is a third flowchart of the dynamic control method of the cargo compartment door according to the present application, based on the above-mentioned embodiments, the method further comprises:

[0063] S20, acquiring the minimum power storage door among the four side doors and the bottom door;

[0064] S30, detecting whether the minimum power storage door meets the estimated power consumption.

[0065] Optionally, in the present embodiment, when the minimum power storage door meets the estimated power consumption, and the minimum power storage door is the top door, the battery module contained in the corresponding door of the minimum power storage door among the four side doors and the bottom door supplies power to the aircraft.

[0066] Optionally, in the present embodiment, when the minimum power storage door meets the estimated power consumption, and the minimum power storage door is not the top door, the battery module contained in any door among the four side doors and the bottom door supplies power to the aircraft.

[0067] Figure 4 FIG. 4 is a fourth flowchart of the dynamic control method of the cargo compartment door according to the present application, based on the above-mentioned embodiments, the method further comprises:

[0068] S40, when the minimum power storage door is the side door, and the minimum power storage door does not meet the estimated power consumption, it is set that when the side door is used for taking out the goods, the minimum power storage side door, the other three side doors, and the bottom door contain the battery module, and the power supply priority is set from high to low.

[0069] S50, when the minimum power storage door is the side door, and the minimum power storage door does not meet the estimated power consumption, it is set that when the bottom door is used for taking out the goods, the minimum power storage side door, the bottom door, and the other three side doors contain the battery module, and the power supply priority is set from high to low.

[0070] Optionally, in the embodiment, when the minimum power storage door is a side door and the minimum power storage door does not meet the estimated power consumption, the power supply priority of the battery modules contained in the minimum power storage side door, the other three side doors and the bottom door is set from high to low when the side door is set for picking up. Among the other three side doors, the power supply priority of the two side doors adjacent to the minimum power storage side door is set to be higher than that of the side door opposite to the minimum power storage side door.

[0071] Optionally, in the embodiment, when the minimum power storage door is a side door and the minimum power storage door does not meet the estimated power consumption, the power supply priority of the battery modules contained in the minimum power storage side door, the other three side doors and the bottom door is set from high to low when the side door is set for picking up. Among the other three side doors, the power supply priority of the two side doors adjacent to the minimum power storage side door is set to be higher than that of the side door opposite to the minimum power storage side door.

[0072] Figure 5 The fifth flowchart of the warehouse door dynamic control method is based on the above-mentioned embodiments, and the method further comprises:

[0073] S60, when the minimum power storage door is a bottom door and the minimum power storage door does not meet the estimated power consumption, the power supply priority of the battery modules contained in the four side doors is determined to be higher than that of the battery modules contained in the bottom door when the side door is set for picking up.

[0074] S70, when the minimum power storage door is a bottom door and the minimum power storage door does not meet the estimated power consumption, the power supply priority of the battery modules contained in the bottom door is determined to be higher than that of the battery modules contained in the four side doors when the bottom door is set for picking up.

[0075] Optionally, in the embodiment, when the minimum power storage door is a bottom door and the minimum power storage door does not meet the estimated power consumption, the power supply priority of the battery modules contained in the four side doors is determined to be higher than that of the battery modules contained in the bottom door when the side door is set for picking up. Among them, the side door for picking up is set as the first priority, the other three side doors are set as the second priority, and the bottom door is set as the third priority.

[0076] Optionally, in the embodiment, when the minimum power storage door is a bottom door and the minimum power storage door does not meet the estimated power consumption, the power supply priority of the battery modules contained in the bottom door is determined to be higher than that of the battery modules contained in the four side doors when the bottom door is set for picking up. Among them, the bottom door is set as the first priority, and the other four side doors are set as the second priority.

[0077] Based on the above embodiments, the present invention further proposes a dynamic control device for a cargo warehouse door, the device comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein when the computer program is executed by the processor, the following is achieved:

[0078] When the aircraft takes off with the cargo hold, the stored power of four side doors and one bottom door of the cargo hold is obtained, wherein the four side doors and the bottom door all contain battery modules;

[0079] When the estimated power consumption of the current voyage exceeds the storage power of a single side door or the bottom door, obtaining the cargo hold opening surface set for the target storage cabinet of the current voyage;

[0080] When setting up the bottom door pickup, the power supply priority of the battery module contained in the bottom door is determined to be higher than the power supply priority of the battery modules contained in the four side doors. When setting up the side door pickup, the power supply priority of the battery modules contained in the four side doors is determined to be higher than the power supply priority of the battery modules contained in the bottom door.

[0081] When the aircraft lands with the cargo hold, if the cargo is to be picked up through the bottom door, the bottom door will support the cargo and transfer it into the target storage cabinet. If the cargo is to be picked up through the side door, the side door with the lowest power will be lowered to support the cargo and transfer it into the target storage cabinet.

[0082] Optionally, when the computer program is executed by the processor, it implements:

[0083] Detecting the current compartment door of the aircraft;

[0084] When it is determined that the goods are to be placed through the bottom door, the bottom door carrying the fully charged battery module supports the goods to be transferred into the cargo warehouse, and the cargo warehouse is closed by the bottom door. When it is determined that the goods are to be placed through the side door, the side door carrying the fully charged battery module supports the goods to be transferred into the cargo warehouse, and the cargo warehouse is closed by erecting the side door.

[0085] Optionally, when the computer program is executed by the processor, it implements:

[0086] Obtaining the smallest power storage door among the four side doors and the bottom door;

[0087] Detect whether the minimum power storage compartment door meets the estimated power consumption.

[0088] Optionally, when the computer program is executed by the processor, it implements:

[0089] In the case that the minimum power storage compartment door is a side compartment door and the minimum power storage compartment door does not satisfy the estimated power consumption, when the side door is set for picking up, the power supply priorities of the battery modules included in the minimum power storage side compartment door, the other three side compartment doors and the bottom compartment door are set from high to low.

[0090] In the case that the minimum power storage compartment door is a side compartment door and the minimum power storage compartment door does not satisfy the estimated power consumption, when the bottom door is set for picking up, the power supply priorities of the battery modules included in the minimum power storage side compartment door, the bottom compartment door and the other three side compartment doors are set from high to low.

[0091] In the case that the minimum power storage compartment door is a bottom compartment door and the minimum power storage compartment door does not satisfy the estimated power consumption, when the side door is set for picking up, it is determined that the power supply priorities of the battery modules included in the four side compartment doors are higher than the power supply priorities of the battery modules included in the bottom compartment door.

[0092] In the case that the minimum power storage compartment door is a bottom compartment door and the minimum power storage compartment door does not satisfy the estimated power consumption, when the bottom door is set for picking up, it is determined that the power supply priorities of the battery modules included in the bottom compartment door are higher than the power supply priorities of the battery modules included in the four side compartment doors.

[0093] It should be noted that the device embodiment and the method embodiment described above belong to the same concept, and the specific implementation process is detailed in the method embodiment, and the technical features in the method embodiment are all applicable in the device embodiment, which will not be repeated here.

[0094] Based on the above embodiments, the application further provides a computer readable storage medium, and the computer readable storage medium stores a warehouse door dynamic control program. When the warehouse door dynamic control program is executed by a processor, the steps of the warehouse door dynamic control method according to any one of the above embodiments are implemented.

[0095] It should be noted that the medium embodiment and the method embodiment described above belong to the same concept, and the specific implementation process is detailed in the method embodiment, and the technical features in the method embodiment are all applicable in the medium embodiment, which will not be repeated here.

[0096] It should be noted that in this document, the terms "comprising", "including", or any other variant thereof are intended to cover non-exclusive inclusions, so that a process, method, article or device including a series of elements not only includes those elements, but also includes other elements not explicitly listed or inherent to such a process, method, article or device. Without more limitations, the element defined by the statement "including a" does not exclude the presence of another identical element in the process, method, article or device including the element.

[0097] The above-mentioned embodiment numbers of the present application are only for description, and do not represent the advantages and disadvantages of the embodiments.

[0098] Through the above description of the embodiments, those skilled in the art can clearly understand that the above-mentioned embodiment methods can be realized by means of software and the necessary general hardware platform, of course, they can also be realized by hardware, but in many cases, the former is a better embodiment. Based on such understanding, the technical solutions of the present application can be embodied in the form of a software product, which is stored in a storage medium (such as ROM / RAM, magnetic disk, optical disk), and includes a plurality of instructions for making a terminal (which can be a mobile phone, computer, server, air conditioner, or network device, etc.) execute the methods described in various embodiments of the present application.

[0099] The embodiments of the present application are described above in combination with the drawings, but the present application is not limited to the above-mentioned specific embodiments, and the above-mentioned specific embodiments are only illustrative, not restrictive. Those skilled in the art can make many forms under the inspiration of the present application without departing from the scope of the present application and the scope protected by the claims.

Claims

1. A method for dynamic control of a warehouse door, characterized in that: The method comprises: When the aircraft takes off with the cargo hold, the stored power of four side doors and one bottom door of the cargo hold is obtained, wherein the four side doors and the bottom door all contain battery modules; When the estimated power consumption of the current voyage exceeds the storage power of a single side door or the bottom door, obtaining the cargo hold opening surface set for the target storage cabinet of the current voyage; When setting up the bottom door pickup, the power supply priority of the battery module contained in the bottom door is determined to be higher than the power supply priority of the battery modules contained in the four side doors. When setting up the side door pickup, the power supply priority of the battery modules contained in the four side doors is determined to be higher than the power supply priority of the battery modules contained in the bottom door. When the aircraft lands with the cargo hold, if the cargo is to be picked up through the bottom door, the bottom door will support the cargo and transfer it into the target storage cabinet. If the cargo is to be picked up through the side door, the side door with the lowest power will be lowered to support the cargo and transfer it into the target storage cabinet.

2. The method for dynamic control of a cargo warehouse door according to claim 1, characterized in that: When the aircraft takes off with the cargo hold, the stored power of the four side doors and one bottom door of the cargo hold is obtained, wherein the four side doors and the bottom door all include battery modules, which previously includes: Detecting the current compartment door of the aircraft; When it is determined that the goods are to be placed through the bottom door, the bottom door carrying the fully charged battery module supports the goods to be transferred into the cargo warehouse, and the cargo warehouse is closed by the bottom door. When it is determined that the goods are to be placed through the side door, the side door carrying the fully charged battery module supports the goods to be transferred into the cargo warehouse, and the cargo warehouse is closed by erecting the side door.

3. The method for dynamic control of a cargo warehouse door according to claim 1, characterized in that: The method further comprises: Obtaining the smallest power storage door among the four side doors and the bottom door; Detect whether the minimum power storage compartment door meets the estimated power consumption.

4. The method for dynamic control of a cargo warehouse door according to claim 3, characterized in that: The method further comprises: When the minimum power storage door is the bottom door and the minimum power storage door does not meet the estimated power consumption, when setting the side door for picking up items, it is determined that the power supply priority of the battery modules included in the four side doors is higher than the power supply priority of the battery modules included in the bottom door; When the minimum power storage door is the bottom door, and the minimum power storage door does not meet the estimated power consumption, when setting the bottom door to pick up items, it is determined that the power supply priority of the battery module contained in the bottom door is higher than the power supply priority of the battery modules contained in the four side doors.

5. A dynamic control device for a cargo warehouse door, characterized in that: The device includes a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein when the computer program is executed by the processor, the computer program implements: When the aircraft takes off with the cargo hold, the stored power of four side doors and one bottom door of the cargo hold is obtained, wherein the four side doors and the bottom door all contain battery modules; When the estimated power consumption of the current voyage exceeds the storage power of a single side door or the bottom door, obtaining the cargo hold opening surface set for the target storage cabinet of the current voyage; When setting up the bottom door pickup, the power supply priority of the battery module contained in the bottom door is determined to be higher than the power supply priority of the battery modules contained in the four side doors. When setting up the side door pickup, the power supply priority of the battery modules contained in the four side doors is determined to be higher than the power supply priority of the battery modules contained in the bottom door. When the aircraft lands with the cargo hold, if the cargo is to be picked up through the bottom door, the bottom door will support the cargo and transfer it into the target storage cabinet. If the cargo is to be picked up through the side door, the side door with the lowest power will be lowered to support the cargo and transfer it into the target storage cabinet.

6. The dynamic control device for cargo hold doors according to claim 5, characterized in that: When the computer program is executed by the processor, it realizes: Detecting the current compartment door of the aircraft; When it is determined that the goods are to be placed through the bottom door, the bottom door carrying the fully charged battery module supports the goods to be transferred into the cargo warehouse, and the cargo warehouse is closed by the bottom door. When it is determined that the goods are to be placed through the side door, the side door carrying the fully charged battery module supports the goods to be transferred into the cargo warehouse, and the cargo warehouse is closed by erecting the side door.

7. The dynamic control device for cargo hold doors according to claim 6, characterized in that: When the computer program is executed by the processor, it realizes: Obtaining the smallest power storage door among the four side doors and the bottom door; Detect whether the minimum power storage compartment door meets the estimated power consumption.

8. The dynamic control device for cargo hold doors according to claim 7, characterized in that: When the computer program is executed by the processor, it realizes: When the minimum power storage door is the bottom door and the minimum power storage door does not meet the estimated power consumption, when setting the side door for picking up items, it is determined that the power supply priority of the battery modules included in the four side doors is higher than the power supply priority of the battery modules included in the bottom door; When the minimum power storage door is the bottom door, and the minimum power storage door does not meet the estimated power consumption, when setting the bottom door to pick up items, it is determined that the power supply priority of the battery module contained in the bottom door is higher than the power supply priority of the battery modules contained in the four side doors.

9. A computer-readable storage medium, characterized in that The computer-readable storage medium stores a cargo hold door dynamic control program, which, when executed by a processor, implements the steps of the cargo hold door dynamic control method according to any one of claims 1 to 4.

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