A high-temperature battery cell replacement control method, device and computer readable storage medium

Abstract

The application discloses a high-temperature battery cell replacement control method and device and a computer readable storage medium, and relates to the field of aviation safety control. The method comprises the following steps: when a high-temperature battery cell exists in a battery compartment of an aircraft, the aircraft is controlled to transfer the high-temperature battery cell to a storage compartment of the aircraft through a first channel prearranged in the aircraft; the aircraft is controlled to transfer goods in the storage compartment to the battery compartment through a second channel prearranged in the aircraft; when the battery cell temperature of the high-temperature battery cell meets preset temperature conditions, the aircraft is controlled to throw the storage compartment out; and when the throwing movement of the storage compartment meets preset parameter conditions, the storage compartment is controlled to open a parachute. The application realizes a safer scheme of high-temperature battery cell air replacement and slow descent, effectively reduces the harmfulness of high-temperature battery cells to transported goods or external environment without affecting the transportation of goods, and guarantees the safety of the aircraft and the ground.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of unmanned aerial vehicles, and in particular to a high-temperature battery cell replacement control method, device and computer readable storage medium. BACKGROUND

[0002] In the prior art, with the continuous development of unmanned aerial vehicle technology, the flight safety of the aerial vehicle is increasingly important.

[0003] Currently, during the execution of a flight task by an aerial vehicle, if a battery pack of the aerial vehicle fails, for example, if an abnormal high temperature occurs in a certain battery cell in the battery pack, the aerial vehicle will generally immediately perform a return operation or a landing operation, which will cause the current flight task to be terminated; for another example, the aerial vehicle throws a high-temperature battery cell to the outside, but the high-temperature battery cell may increase the fire hazard of the external environment.

[0004] Therefore, in the flight process of an unmanned aerial vehicle, how to effectively and safely handle a high-temperature battery cell in the case of an abnormal high-temperature battery cell has become a technical problem to be solved. SUMMARY

[0005] In order to solve the above technical defects in the prior art, the present application provides a high-temperature battery cell replacement control method, which comprises:

[0006] When a high-temperature battery cell exists in a battery compartment of an aerial vehicle, a first transfer instruction is generated, the first transfer instruction being used to control the aerial vehicle to transfer the high-temperature battery cell to a storage compartment of the aerial vehicle through a first channel pre-set in the aerial vehicle;

[0007] A second transfer instruction corresponding to the first transfer instruction is generated, the second transfer instruction being used to control the aerial vehicle to transfer goods in the storage compartment to the battery compartment through a second channel pre-set in the aerial vehicle;

[0008] When a battery cell temperature of the high-temperature battery cell meets a pre-set temperature condition, a throwing instruction is generated, the throwing instruction being used to control the aerial vehicle to throw the storage compartment to the outside;

[0009] When a throwing movement of the storage compartment meets a pre-set parameter condition, a slow descent instruction is generated and sent to the storage compartment, the slow descent instruction being used to control the storage compartment to open a parachute.

[0010] Optionally, the method further comprises:

[0011] When the battery compartment is loaded to the aerial vehicle, a storage compartment loading state of the storage compartment is acquired;

[0012] When the battery compartment has completed loading, the first channel of the battery compartment to the storage compartment is established.

[0013] Optionally, the method further comprises:

[0014] When the storage compartment is loaded to the aircraft, a battery compartment loading state of the battery compartment is acquired;

[0015] When the battery compartment has completed loading, the second channel of the storage compartment to the battery compartment is established.

[0016] Optionally, when the cell temperature of the high-temperature cell meets the preset temperature condition, a jettison instruction is generated, and the jettison instruction is used to control the aircraft to jettison the storage compartment outward, and specifically comprises:

[0017] When the cell temperature of the high-temperature cell meets the preset temperature condition, the current flight state is adjusted according to the current ground state;

[0018] When the flight state is adjusted to meet the preset jettison speed, jettison direction and jettison height, the jettison instruction is generated.

[0019] Optionally, when the jettison movement of the storage compartment meets the preset parameter condition, a slow descent instruction is generated and sent to the storage compartment, and the slow descent instruction is used to control the storage compartment to open a parachute, and specifically comprises:

[0020] Real-time movement parameters transmitted by the storage compartment are acquired, wherein the real-time movement parameters include movement speed, movement direction and real-time height;

[0021] When the movement speed, the movement direction and the real-time height calculated according to the ground state meet the parameter condition, the slow descent instruction is generated.

[0022] The application further provides a high-temperature cell replacement 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:

[0023] When there is a high-temperature cell in the battery compartment of the aircraft, a first transfer instruction is generated, and the first transfer instruction is used to control the aircraft to transfer the high-temperature cell to the storage compartment of the aircraft through a first channel preset in the aircraft;

[0024] A second transfer instruction corresponding to the first transfer instruction is generated, and the second transfer instruction is used to control the aircraft to transfer goods in the storage compartment to the battery compartment through a second channel preset in the aircraft;

[0025] When the temperature of the high-temperature battery cell meets the preset temperature conditions, a throwing command is generated. The throwing command is used to control the aircraft to throw the storage compartment outward.

[0026] When the throwing motion of the storage compartment meets the preset parameter conditions, a slow descent command is generated and sent to the storage compartment. The slow descent command is used to control the storage compartment to deploy its parachute.

[0027] Optionally, the computer program is implemented when executed by the processor as follows:

[0028] When the battery compartment is loaded into the aircraft, the loading status of the storage compartment is obtained;

[0029] When the storage compartment has been loaded, establish the first channel from the battery compartment to the storage compartment;

[0030] or,

[0031] When the storage compartment is loaded into the aircraft, the battery compartment loading status is obtained;

[0032] When the battery compartment is fully loaded, a second channel is established from the storage compartment to the battery compartment.

[0033] Optionally, the computer program is implemented when executed by the processor as follows:

[0034] When the temperature of the high-temperature battery cell meets the preset temperature conditions, the current flight status is adjusted according to the current ground conditions.

[0035] When the flight state is adjusted to meet the preset throwing speed, throwing direction and throwing height, the throwing command is generated.

[0036] Optionally, the computer program is implemented when executed by the processor as follows:

[0037] The real-time motion parameters transmitted by the storage compartment are obtained, wherein the real-time motion parameters include motion speed, motion direction and real-time height;

[0038] When the calculated movement speed, movement direction, and real-time height based on the ground conditions meet the parameter conditions, the descent command is generated.

[0039] The present invention also proposes a computer-readable storage medium storing a high-temperature battery cell replacement control program, which, when executed by a processor, implements the steps of the high-temperature battery cell replacement control method as described in any of the preceding claims.

[0040] The present invention provides a high-temperature battery cell replacement control method, device, and computer-readable storage medium. When a high-temperature battery cell is present in the battery compartment of an aircraft, a first transfer command is generated. This first transfer command controls the aircraft to transfer the high-temperature battery cell to the aircraft's storage compartment via a first channel pre-set within the aircraft. A second transfer command corresponding to the first transfer command is generated. This second transfer command controls the aircraft to transfer cargo from the storage compartment to the battery compartment via a second channel pre-set within the aircraft. When the temperature of the high-temperature battery cell meets preset temperature conditions, a throwing command is generated. This throwing command controls the aircraft to throw the storage compartment outwards. When the throwing motion of the storage compartment meets preset parameter conditions, a deceleration command is generated and sent to the storage compartment. This deceleration command controls the storage compartment to deploy its parachute. The present invention provides a safer solution for in-flight replacement and deceleration of high-temperature battery cells. Without affecting normal aircraft flight or cargo transportation, it effectively reduces the hazards of high-temperature battery cells to transported cargo or the external environment, while ensuring the safety of the aircraft and the ground. Attached Figure Description

[0041] The present invention will be further described below with reference to the accompanying drawings and embodiments. In the accompanying drawings:

[0042] Figure 1 This is the first flowchart of the high-temperature cell replacement control method of the present invention;

[0043] Figure 2 This is the second flowchart of the high-temperature cell replacement control method of the present invention;

[0044] Figure 3 This is the third flowchart of the high-temperature cell replacement control method of the present invention;

[0045] Figure 4 This is the fourth flowchart of the high-temperature cell replacement control method of the present invention;

[0046] Figure 5 This is the fifth flowchart of the high-temperature cell replacement control method of the present invention. Detailed Implementation

[0047] It should be understood that the specific embodiments described herein are for illustrative purposes only and are not intended to limit the scope of the invention.

[0048] In the following description, the use of suffixes such as "module," "part," or "unit" to denote elements is solely for the purpose of illustrative purposes and has no specific meaning in itself. Therefore, "module," "part," or "unit" may be used interchangeably.

[0049] Figure 1This is a first flowchart of the high-temperature battery cell replacement control method of the present invention. This embodiment proposes a high-temperature battery cell replacement control method, which includes:

[0050] S1. When there is a high-temperature battery cell in the battery compartment of the aircraft, a first transfer command is generated. The first transfer command is used to control the aircraft to transfer the high-temperature battery cell to the storage compartment of the aircraft through a first channel preset in the aircraft.

[0051] S2. Generate a second transfer instruction corresponding to the first transfer instruction. The second transfer instruction is used to control the aircraft to transfer the goods in the storage compartment to the battery compartment through a second channel preset in the aircraft.

[0052] S3. When the cell temperature of the high-temperature battery cell meets the preset temperature conditions, a throwing command is generated. The throwing command is used to control the aircraft to throw the storage compartment outward.

[0053] S4. When the throwing motion of the storage compartment meets the preset parameter conditions, a slow descent command is generated and sent to the storage compartment. The slow descent command is used to control the storage compartment to open its parachute.

[0054] Optionally, in this embodiment, the first channel and the second channel are different unidirectional channels. The first channel incorporates a first unidirectional track or a first unidirectional traction component from the battery compartment to the storage compartment. This first unidirectional track or first unidirectional traction component has a first fixing interface or a first traction interface that matches the battery cell or battery pack. The first transfer command includes a first interface command and a first transfer command. The first interface command controls the first unidirectional track or the first unidirectional traction component to fix or traction the current high-temperature battery cell or the battery pack containing the high-temperature battery cell through the first fixing interface or the first traction interface. The first transfer command controls the first unidirectional track or the first unidirectional traction component to transfer the current high-temperature battery cell or the battery pack containing the high-temperature battery cell from the battery compartment to the storage compartment. In this embodiment, the second channel incorporates a second unidirectional track or a second unidirectional traction component that connects the storage compartment to the battery compartment. The second unidirectional track or the second unidirectional traction component has a second fixing interface or a second traction interface that matches the goods or goods packaging. The second transfer command includes a second interface command and a second transfer command. The second interface command controls the second unidirectional track or the second unidirectional traction component to fix or traction the current goods or goods packaging through the second fixing interface or the second traction interface. The second transfer command controls the second unidirectional track or the second unidirectional traction component to transfer the current goods or goods packaging from the storage compartment to the battery compartment.

[0055] Optionally, in this embodiment, the first channel and the second channel are a shared channel, which has two built-in unidirectional transfer paths. The first transfer path includes a first unidirectional track or a first unidirectional traction component from the battery compartment to the storage compartment. The first unidirectional track or the first unidirectional traction component has a first fixing interface or a first traction interface that matches the battery cell or battery pack. The first transfer command includes a first interface command and a first transfer command. The first interface command controls the first unidirectional track or the first unidirectional traction component to fix or traction the current high-temperature battery cell or the battery pack containing the high-temperature battery cell through the first fixing interface or the first traction interface. The first transfer command controls the first unidirectional track or the first unidirectional traction component to transfer the current high-temperature battery cell or the battery pack containing the high-temperature battery cell from the battery compartment to the storage compartment. In this embodiment, the second transfer path includes a second unidirectional track or a second unidirectional traction component from the storage compartment to the battery compartment. The second unidirectional track or the second unidirectional traction component has a second fixing interface or a second traction interface that matches the goods or goods packaging. The second transfer command includes a second interface command and a second transfer command. The second interface command is used to control the second unidirectional track or the second unidirectional traction component to fix or traction the current goods or goods packaging through the second fixing interface or the second traction interface. The second transfer command is used to control the second unidirectional track or the second unidirectional traction component to transfer the current goods or goods packaging from the storage compartment to the battery compartment.

[0056] Optionally, in this embodiment, the first channel and the second channel are a shared channel, which incorporates a bidirectional transfer path. The first-direction transfer path includes a bidirectional track or bidirectional traction assembly from the battery compartment to the storage compartment. This bidirectional track or traction assembly has a first fixing interface or a first traction interface that matches the battery cell or battery pack. The first transfer command includes a first interface command and a first transfer command. The first interface command controls the bidirectional track or traction assembly to fix or traction the current high-temperature battery cell or battery pack containing the high-temperature battery cell through the first fixing interface or the first traction interface. The first transfer command controls the bidirectional track or traction assembly to transfer the current high-temperature battery cell or battery pack containing the high-temperature battery cell from the battery compartment to the storage compartment. In this embodiment, the transfer path in the second direction includes the same bidirectional track or bidirectional traction assembly as described above, which runs from the storage compartment to the battery compartment. The bidirectional track or bidirectional traction assembly has a second fixing interface or a second traction interface that matches the goods or goods packaging. The second transfer command includes a second interface command and a second transfer command. The second interface command is used to control the bidirectional track or bidirectional traction assembly to fix or pull the current goods or goods packaging through the second fixing interface or the second traction interface, while the second transfer command is used to control the bidirectional track or bidirectional traction assembly to transfer the current goods or goods packaging from the storage compartment to the battery compartment.

[0057] The beneficial effects of implementing this embodiment are as follows: When a high-temperature battery cell is present in the aircraft's battery compartment, a first transfer command is generated. This first transfer command controls the aircraft to transfer the high-temperature battery cell to the aircraft's storage compartment via a first channel pre-set within the aircraft. A second transfer command corresponding to the first transfer command is generated. This second transfer command controls the aircraft to transfer cargo from the storage compartment to the battery compartment via a second channel pre-set within the aircraft. When the temperature of the high-temperature battery cell meets a preset temperature condition, a throwing command is generated. This throwing command controls the aircraft to throw the storage compartment outwards. When the throwing motion of the storage compartment meets preset parameter conditions, a deceleration command is generated and sent to the storage compartment. This deceleration command controls the storage compartment to deploy its parachute. This achieves a safer solution for in-flight replacement and deceleration of high-temperature battery cells, effectively reducing the harm of high-temperature battery cells to transported cargo or the external environment without affecting the normal flight of the aircraft or cargo transportation, while ensuring the safety of the aircraft and the ground.

[0058] Figure 2 This is a second flowchart of the high-temperature cell replacement control method of the present invention. Based on the above embodiments, the method further includes:

[0059] S01. When the battery compartment is loaded into the aircraft, obtain the storage compartment loading status;

[0060] S02. When the storage compartment has been loaded, establish the first channel from the battery compartment to the storage compartment.

[0061] Optionally, in this embodiment, the first channel and the second channel are a shared channel, which has two built-in unidirectional transfer paths, or it has one built-in bidirectional transfer path. When the storage compartment has been loaded, the current cargo size information and cargo structure information in the storage compartment are obtained, and the aforementioned shared channel is established based on the cargo size information and cargo structure information.

[0062] Figure 3 This is the third flowchart of the high-temperature cell replacement control method of the present invention. Based on the above embodiments, the method further includes:

[0063] S03. When the storage compartment is loaded into the aircraft, obtain the battery compartment loading status of the battery compartment;

[0064] S04. When the battery compartment has been loaded, establish the second channel from the storage compartment to the battery compartment.

[0065] Optionally, in this embodiment, the first channel and the second channel are a shared channel, which has two built-in unidirectional transfer paths, or it has one built-in bidirectional transfer path. When the battery compartment has been loaded, the cell size information, cell structure information, battery pack size information, and battery pack structure information of the current cells or battery pack in the battery compartment are obtained, and the aforementioned shared channel is established based on the cell size information, cell structure information, battery pack size information, and battery pack structure information.

[0066] Figure 4 This is the fourth flowchart of the high-temperature battery cell replacement control method of the present invention. Based on the above embodiments, when the battery cell temperature of the high-temperature battery cell meets the preset temperature conditions, a throwing command is generated. The throwing command is used to control the aircraft to throw the storage compartment outward, specifically including:

[0067] S31. When the temperature of the high-temperature battery cell meets the preset temperature conditions, adjust the current flight state according to the current ground conditions.

[0068] S32. When the flight state is adjusted to meet the preset throwing speed, throwing direction and throwing height, the throwing command is generated.

[0069] Optionally, in this embodiment, the current ground state is the detection result of the area range of the ground, wherein the detection target is the safe landing area or the preset area containing the high-temperature battery cell disposal point.

[0070] Optionally, in this embodiment, since the storage compartment itself does not have a propulsion component, in order to enable the storage compartment to move freely to a safe landing area or a preset area containing a high-temperature battery cell disposal point, this embodiment first adjusts the current flight state to a flight speed, flight direction, and flight height corresponding to preset throwing speed, throwing direction, and throwing height before throwing the storage compartment. Then, the above-mentioned throwing command is generated and the throwing is executed, so that at the moment the storage compartment is thrown, its initial motion parameters are determined to include the above-mentioned throwing speed, throwing direction, and throwing height.

[0071] Figure 5 This is the fifth flowchart of the high-temperature battery cell replacement control method of the present invention. Based on the above embodiment, when the throwing motion of the storage compartment meets the preset parameter conditions, a slow descent command is generated and sent to the storage compartment. The slow descent command is used to control the storage compartment to deploy its parachute, specifically including:

[0072] S41. Obtain real-time motion parameters transmitted by the storage compartment, wherein the real-time motion parameters include motion speed, motion direction and real-time height;

[0073] S42. When the calculated movement speed, movement direction, and real-time height based on the ground conditions meet the parameter conditions, the descent command is generated.

[0074] Optionally, in this embodiment, due to the influence of wind direction, wind speed, and the wind resistance of the storage compartment itself on the movement trajectory of the storage compartment, the initial movement parameters alone cannot guarantee that the storage compartment can move freely to a safe landing area or a preset area containing the high-temperature battery cell disposal point. Therefore, in this embodiment, for the movement process of the storage compartment, by reasonably selecting the timing of parachute release, the storage compartment, under the slow descent effect of the parachute, can slowly descend to a safe landing area or a preset area containing the high-temperature battery cell disposal point. It can be seen that the method of releasing the parachute during the throwing motion adopted in this embodiment can, on the one hand, adjust the real-time movement trajectory of the storage compartment, and on the other hand, implement a slow descent of the storage compartment, improve the structural safety of the storage compartment, and avoid greater safety hazards caused by the built-in high-temperature battery cells.

[0075] Based on the above embodiments, the present invention also proposes a high-temperature battery cell replacement control device, which includes a memory, a processor, and a computer program stored in the memory and executable on the processor. When the computer program is executed by the processor, it implements the following:

[0076] When there are high-temperature battery cells in the battery compartment of the aircraft, a first transfer command is generated. The first transfer command is used to control the aircraft to transfer the high-temperature battery cells to the storage compartment of the aircraft through a first channel preset in the aircraft.

[0077] Generate a second transfer instruction corresponding to the first transfer instruction. The second transfer instruction is used to control the aircraft to transfer the goods in the storage compartment to the battery compartment through a second channel preset in the aircraft.

[0078] When the temperature of the high-temperature battery cell meets the preset temperature conditions, a throwing command is generated. The throwing command is used to control the aircraft to throw the storage compartment outward.

[0079] When the throwing motion of the storage compartment meets the preset parameter conditions, a slow descent command is generated and sent to the storage compartment. The slow descent command is used to control the storage compartment to deploy its parachute.

[0080] Optionally, the computer program is implemented when executed by the processor as follows:

[0081] When the battery compartment is loaded into the aircraft, the loading status of the storage compartment is obtained;

[0082] When the storage compartment has been loaded, establish the first channel from the battery compartment to the storage compartment;

[0083] or,

[0084] When the storage compartment is loaded into the aircraft, the battery compartment loading status is obtained;

[0085] When the battery compartment is fully loaded, a second channel is established from the storage compartment to the battery compartment.

[0086] Optionally, the computer program is implemented when executed by the processor as follows:

[0087] When the temperature of the high-temperature battery cell meets the preset temperature conditions, the current flight status is adjusted according to the current ground conditions.

[0088] When the flight state is adjusted to meet the preset throwing speed, throwing direction and throwing height, the throwing command is generated.

[0089] Optionally, the computer program is implemented when executed by the processor as follows:

[0090] The real-time motion parameters transmitted by the storage compartment are obtained, wherein the real-time motion parameters include motion speed, motion direction and real-time height;

[0091] When the calculated movement speed, movement direction, and real-time height based on the ground conditions meet the parameter conditions, the descent command is generated.

[0092] It should be noted that the above-described device embodiments and method embodiments belong to the same concept. The specific implementation process can be found in the method embodiments, and the technical features in the method embodiments are also applicable to the device embodiments, which will not be repeated here.

[0093] Based on the above embodiments, the present invention also proposes a computer-readable storage medium storing a high-temperature battery cell replacement control program, which, when executed by a processor, implements the steps of the high-temperature battery cell replacement control method as described in any of the above embodiments.

[0094] It should be noted that the above-described medium embodiments and method embodiments belong to the same concept. The specific implementation process can be found in the method embodiments, and the technical features in the method embodiments are also applicable to the medium embodiments, which will not be repeated here.

[0095] It should be noted that, in this document, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. Unless otherwise specified, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, method, article, or apparatus that includes that element.

[0096] The sequence numbers of the above embodiments of the present invention are for descriptive purposes only and do not represent the superiority or inferiority of the embodiments.

[0097] Through the above description of the embodiments, those skilled in the art can clearly understand that the methods of the above embodiments can be implemented by means of software plus necessary general-purpose hardware platforms. Of course, they can also be implemented by hardware, but in many cases the former is a better implementation method. Based on this understanding, the technical solution of the present invention, in essence, or the part that contributes to the prior art, can be embodied in the form of a software product. This computer software product is stored in a storage medium (such as ROM / RAM, magnetic disk, optical disk), and includes several instructions to cause a terminal (which may be a mobile phone, computer, server, air conditioner, or network device, etc.) to execute the methods described in the various embodiments of the present invention.

[0098] The embodiments of the present invention have been described above with reference to the accompanying drawings. However, the present invention is not limited to the specific embodiments described above. The specific embodiments described above are merely illustrative and not restrictive. Those skilled in the art can make many other forms under the guidance of the present invention without departing from the spirit and scope of the claims. All of these forms are within the protection scope of the present invention.

Claims

1. A high-temperature battery cell replacement control method, characterized in that, The method includes: When there are high-temperature battery cells in the battery compartment of the aircraft, a first transfer command is generated. The first transfer command is used to control the aircraft to transfer the high-temperature battery cells to the storage compartment of the aircraft through a first channel preset in the aircraft. Generate a second transfer instruction corresponding to the first transfer instruction. The second transfer instruction is used to control the aircraft to transfer the goods in the storage compartment to the battery compartment through a second channel preset in the aircraft. When the temperature of the high-temperature battery cell meets the preset temperature conditions, a throwing command is generated. The throwing command is used to control the aircraft to throw the storage compartment outward. When the throwing motion of the storage compartment meets the preset parameter conditions, a slow descent command is generated and sent to the storage compartment. The slow descent command is used to control the storage compartment to deploy its parachute.

2. The high-temperature cell replacement control method according to claim 1, characterized in that, The method further includes: When the battery compartment is loaded into the aircraft, the loading status of the storage compartment is obtained; When the storage compartment is fully loaded, the first channel from the battery compartment to the storage compartment is established.

3. The high-temperature cell replacement control method according to claim 1, characterized in that, The method further includes: When the storage compartment is loaded into the aircraft, the battery compartment loading status is obtained; When the battery compartment is fully loaded, a second channel is established from the storage compartment to the battery compartment.

4. The high-temperature cell replacement control method according to claim 3, characterized in that, When the temperature of the high-temperature battery cell meets a preset temperature condition, a throwing command is generated. This throwing command controls the aircraft to throw the storage compartment outwards, specifically including: When the temperature of the high-temperature battery cell meets the preset temperature conditions, the current flight status is adjusted according to the current ground conditions. When the flight state is adjusted to meet the preset throwing speed, throwing direction and throwing height, the throwing command is generated.

5. The high-temperature cell replacement control method according to claim 4, characterized in that, When the throwing motion of the storage compartment meets preset parameter conditions, a descent control command is generated and sent to the storage compartment. The descent control command is used to control the storage compartment to deploy its parachute, specifically including: The real-time motion parameters transmitted by the storage compartment are obtained, wherein the real-time motion parameters include motion speed, motion direction and real-time height; When the calculated movement speed, movement direction, and real-time height based on the ground conditions meet the parameter conditions, the descent command is generated.

6. A high-temperature battery cell replacement control device, characterized in that, The device includes a memory, a processor, and a computer program stored in the memory and executable on the processor, the computer program being executed by the processor to implement: When there are high-temperature battery cells in the battery compartment of the aircraft, a first transfer command is generated. The first transfer command is used to control the aircraft to transfer the high-temperature battery cells to the storage compartment of the aircraft through a first channel preset in the aircraft. Generate a second transfer instruction corresponding to the first transfer instruction. The second transfer instruction is used to control the aircraft to transfer the goods in the storage compartment to the battery compartment through a second channel preset in the aircraft. When the temperature of the high-temperature battery cell meets the preset temperature conditions, a throwing command is generated. The throwing command is used to control the aircraft to throw the storage compartment outward. When the throwing motion of the storage compartment meets the preset parameter conditions, a slow descent command is generated and sent to the storage compartment. The slow descent command is used to control the storage compartment to deploy its parachute.

7. The high-temperature battery cell replacement control device according to claim 6, characterized in that, The computer program is implemented when executed by the processor: When the battery compartment is loaded into the aircraft, the loading status of the storage compartment is obtained; When the storage compartment has been loaded, establish the first channel from the battery compartment to the storage compartment; or, When the storage compartment is loaded into the aircraft, the battery compartment loading status is obtained; When the battery compartment is fully loaded, a second channel is established from the storage compartment to the battery compartment.

8. The high-temperature battery cell replacement control device according to claim 7, characterized in that, The computer program is implemented when executed by the processor: When the temperature of the high-temperature battery cell meets the preset temperature conditions, the current flight status is adjusted according to the current ground conditions. When the flight state is adjusted to meet the preset throwing speed, throwing direction and throwing height, the throwing command is generated.

9. The high-temperature battery cell replacement control device according to claim 8, characterized in that, The computer program is implemented when executed by the processor: The real-time motion parameters transmitted by the storage compartment are obtained, wherein the real-time motion parameters include motion speed, motion direction and real-time height; When the calculated movement speed, movement direction, and real-time height based on the ground conditions meet the parameter conditions, the descent command is generated.

10. A computer-readable storage medium, characterized in that, The computer-readable storage medium stores a high-temperature battery cell replacement control program, which, when executed by a processor, implements the steps of the high-temperature battery cell replacement control method as described in any one of claims 1 to 5.

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