CN116668950B - Target object transferring method and device and nonvolatile storage medium - Google Patents

Target object transferring method and device and nonvolatile storage medium Download PDF

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Publication number
CN116668950B
CN116668950B CN202310951720.5A CN202310951720A CN116668950B CN 116668950 B CN116668950 B CN 116668950B CN 202310951720 A CN202310951720 A CN 202310951720A CN 116668950 B CN116668950 B CN 116668950B
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duration
target object
target
preset
determining
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CN116668950A (en
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孙玉国
刘振宇
崔菁
姚飞
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Zhongwei Zhichuang Beijing Software Technology Co ltd
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Zhongwei Zhichuang Beijing Software Technology Co ltd
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    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
    • H04W4/02—Services making use of location information
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W12/00—Security arrangements; Authentication; Protecting privacy or anonymity
    • H04W12/02—Protecting privacy or anonymity, e.g. protecting personally identifiable information [PII]
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W16/00—Network planning, e.g. coverage or traffic planning tools; Network deployment, e.g. resource partitioning or cells structures
    • H04W16/18—Network planning tools
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W84/00—Network topologies
    • H04W84/02—Hierarchically pre-organised networks, e.g. paging networks, cellular networks, WLAN [Wireless Local Area Network] or WLL [Wireless Local Loop]
    • H04W84/04—Large scale networks; Deep hierarchical networks
    • H04W84/06—Airborne or Satellite Networks
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
    • Y02D30/00—Reducing energy consumption in communication networks
    • Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Computer Security & Cryptography (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)

Abstract

The application discloses a target object transferring method and device and a nonvolatile storage medium. Wherein the method comprises the following steps: determining a first speed expected to be reached by the target object in a first preset duration according to a first preset transfer route, and determining a first position expected to be reached by the target object; under the condition that the first position is in the coverage range of the optical satellite in the first target duration, the target object is instructed to execute camouflage operation; and when the first position is not in the coverage range of the optical satellite in the first target duration or is not in the coverage range of the optical satellite in the second target duration, the target object is instructed to move to the first position, and when the first position is coincident with the end point of the first preset transfer route, the target object is instructed to stop moving. The application solves the technical problem that the safety of the target object is insufficient in the transferring process because the target object cannot be reasonably controlled to be transferred.

Description

Target object transferring method and device and nonvolatile storage medium
Technical Field
The present application relates to the field of data processing technologies, and in particular, to a method and an apparatus for transferring a target object, and a nonvolatile storage medium.
Background
The command needs to be transferred from the site A to the site B, and the reconnaissance of the electronic satellite and the optical satellite can be encountered in the transfer path, so that on one hand, the security requirement of the command post needs to take various measures to avoid the reconnaissance of the satellite, and on the other hand, the command function requirement of the command post keeps external communication in the transfer process, and the command capability cannot be completely lost during the transfer. Therefore, how to reasonably control the transfer of command posts is a problem to be solved.
In view of the above problems, no effective solution has been proposed at present.
Disclosure of Invention
The embodiment of the application provides a target object transferring method and device and a nonvolatile storage medium, which at least solve the technical problem that the safety of a target object is insufficient in the transferring process because the target object cannot be reasonably controlled to be transferred.
According to an aspect of an embodiment of the present application, there is provided a transfer method of a target object, including: determining a first speed which is expected to be reached by the target object in a first preset duration according to a first preset transfer route, and determining a first position which is expected to be reached by the target object according to the first preset transfer route, the first speed and the first preset duration; determining whether the first position is in the coverage area of the optical satellite or not in a first target duration, and indicating the target object to execute camouflage operation until the first position is not in the coverage area of the optical satellite in a second target duration under the condition that the first position is in the coverage area of the optical satellite in the first target duration, wherein the first target duration is the sum of a first preset duration and a duration required by the target object to execute the camouflage operation, and the second target duration is the sum of the first preset duration, a duration required by the target object to execute the camouflage operation and a duration required by the target object to release the camouflage operation; and when the first position is not in the coverage range of the optical satellite in the first target duration or is not in the coverage range of the optical satellite in the second target duration, the target object is instructed to move to the first position, and when the first position is coincident with the end point of the first preset transfer route, the target object is instructed to stop moving.
Optionally, determining whether the first location is within a coverage area of the electronic satellite for a first target duration; under the condition that the first position is in the coverage area of the electronic satellite in the first target time length, indicating the target object to execute electromagnetic silencing operation until the first position is not in the coverage area of the electronic satellite in the first target time length, and recording the starting time and the ending time of the target object to execute the electromagnetic silencing operation; and determining the duration of the electromagnetic silence state of the target object in the first preset transfer line according to the starting time and the ending time.
Optionally, after instructing the target object to perform the electromagnetic silencing operation until the first position is not within the coverage of the electronic satellite for the first target duration, the method further includes: determining a first parameter according to the ratio of a first duration to a second duration, wherein the first duration is the duration of the target object in an electromagnetic silence state in a first preset transfer line, and the second duration is the duration of the target object from a starting point to an end point in the first preset transfer line; determining a second parameter according to the ratio of a third duration to a second duration, wherein the third duration is the duration of communication between the target object and other communicable objects in the first preset transfer line; determining a third parameter according to the ratio of the fourth duration to the second duration, wherein the fourth duration is the duration that the first value is larger than a preset threshold value in the first preset transfer line of the target object, and the first value is the ratio of the distance of communication between the target object and other communicable objects to the average height of the obstacle in the first preset transfer line; determining a first weight corresponding to the first parameter, a second weight corresponding to the second parameter and a third weight corresponding to the third parameter; and according to the first weight, the second weight and the third weight, carrying out weighted summation on the first parameter, the second parameter and the third parameter to obtain a target value, wherein the target value is used for representing the communication capacity of the target object in the first preset transfer line.
Optionally, scoring the preset transfer route at least according to the target value to obtain a scoring result; and displaying the scoring result corresponding to each preset transfer route in the plurality of preset transfer routes.
Optionally, acquiring a second preset transfer route different from the first preset transfer route under the condition that the first position is within the coverage range of the optical satellite within the target preset time period; determining a second speed which is expected to be reached by the target object in a second preset time period according to a second preset transfer route, and determining a second position which is expected to be reached by the target object according to the second preset transfer route, the second speed and the second preset time period; determining whether the second position is in the coverage area of the optical satellite or not in a third target duration, and indicating the target object to execute camouflage operation until the second position is not in the coverage area of the optical satellite in a fourth target duration under the condition that the second position is in the coverage area of the optical satellite in the third target duration, wherein the third target duration is the sum of a second preset duration and a duration required by the target object to execute the camouflage operation, and the fourth target duration is the sum of the second preset duration, a duration required by the target object to execute the camouflage operation and a duration required by the target object to release the camouflage operation; and when the second position is not in the coverage range of the optical satellite in the third target duration or is not in the coverage range of the optical satellite in the fourth target duration, the target object is instructed to move to the second position, and when the second position is coincident with the end point of the second preset transfer route, the target object is instructed to stop moving.
Optionally, determining the first speed that the target object is expected to reach in the first preset duration according to the first preset transfer route includes: acquiring a plurality of longitudinal gradients and a plurality of roll gradients in a first preset transfer route; determining a first average gradient value corresponding to the plurality of longitudinal gradients and a second average gradient value corresponding to the plurality of roll gradients; and determining the first speed at least according to the first average gradient value, the second average gradient value and the soil and pavement materials in the first preset transfer route.
Optionally, before determining whether the first location is within the coverage of the optical satellite for the first target duration, the method further comprises: determining the distance from the optical satellite to the earth center according to the semi-long axis of the optical satellite; determining the true near point angle of the optical satellite according to the eccentricity of the optical satellite; determining a first coordinate of the optical satellite in a satellite orbit coordinate system according to the distance from the optical satellite to the earth center and the true near point angle; converting the first coordinate into a geodetic coordinate system, and obtaining longitude and latitude corresponding to the optical satellite in the geodetic coordinate system; determining the projection position of the optical satellite on the ground according to the longitude and latitude corresponding to the optical satellite; and determining the coverage range of the optical satellite according to the projection position of the optical satellite on the ground and the coverage radius of the optical satellite.
According to still another aspect of the embodiment of the present application, there is also provided a transfer apparatus of a target object, including: the first determining module is used for determining a first speed which is expected to be reached by the target object in a first preset duration according to a first preset transfer route, and determining a first position which is expected to be reached by the target object according to the first preset transfer route, the first speed and the first preset duration; the first control module is used for determining whether the first position is in the coverage area of the optical satellite or not in a first target duration, and indicating the target object to execute camouflage operation until the first position is not in the coverage area of the optical satellite in a second target duration under the condition that the first position is in the coverage area of the optical satellite in the first target duration, wherein the first target duration is the sum of a first preset duration and the duration required by the target object to execute the camouflage operation, and the second target duration is the sum of the first preset duration, the duration required by the target object to execute the camouflage operation and the duration required by the target object to release the camouflage operation; the second control module is used for indicating the target object to move to the first position when the first position is not in the coverage range of the optical satellite in the first target duration or is not in the coverage range of the optical satellite in the second target duration, and indicating the target object to stop moving when the first position is coincident with the end point of the first preset transfer route.
According to still another aspect of the embodiments of the present application, there is also provided a nonvolatile storage medium, the storage medium including a stored program, wherein the program controls a device in which the storage medium is located to execute the above transfer method of the target object when running.
According to still another aspect of the embodiment of the present application, there is also provided an electronic device including: the system comprises a memory and a processor, wherein the processor is used for running a program stored in the memory, and the program runs to execute the transfer method of the target object.
In the embodiment of the application, a first speed which is expected to be reached by a target object in a first preset duration is determined according to a first preset transfer route, and a first position which is expected to be reached by the target object is determined according to the first preset transfer route, the first speed and the first preset duration; determining whether the first position is in the coverage area of the optical satellite or not in a first target duration, and indicating the target object to execute camouflage operation until the first position is not in the coverage area of the optical satellite in a second target duration under the condition that the first position is in the coverage area of the optical satellite in the first target duration, wherein the first target duration is the sum of a first preset duration and a duration required by the target object to execute the camouflage operation, and the second target duration is the sum of the first preset duration, a duration required by the target object to execute the camouflage operation and a duration required by the target object to release the camouflage operation; and when the first position is not in the coverage area of the optical satellite in the first target duration, or the first position is not in the coverage area of the optical satellite in the second target duration, indicating that the target object moves to the first position, and when the first position is coincident with the end point of the first preset transfer route, indicating that the target object stops moving.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this specification, illustrate embodiments of the application and together with the description serve to explain the application and do not constitute a limitation on the application. In the drawings:
FIG. 1 is a flow chart of a method of transferring a target object according to an embodiment of the application;
FIG. 2 is a flow chart of another method of transferring a target object according to an embodiment of the application;
FIG. 3 is a schematic diagram of a command post action state according to an embodiment of the application;
fig. 4 is a block diagram of a transfer apparatus of a target object according to an embodiment of the present application;
fig. 5 is a block diagram of a hardware structure of a computer terminal (or electronic device) of a transfer method of a target object according to an embodiment of the present application.
Detailed Description
In order that those skilled in the art will better understand the present application, a technical solution in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in which it is apparent that the described embodiments are only some embodiments of the present application, not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the present application without making any inventive effort, shall fall within the scope of the present application.
It should be noted that the terms "first," "second," and the like in the description and the claims of the present application and the above figures are used for distinguishing between similar objects and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used may be interchanged where appropriate such that the embodiments of the application described herein may be implemented in sequences other than those illustrated or otherwise described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
According to an embodiment of the present application, there is provided a method embodiment of a target object transferring method, it should be noted that the steps shown in the flowchart of the drawings may be performed in a computer system such as a set of computer executable instructions, and that although a logical order is shown in the flowchart, in some cases, the steps shown or described may be performed in an order different from that shown or described herein.
Fig. 1 is a flowchart of a target object transferring method according to an embodiment of the present application, as shown in fig. 1, the method includes the steps of:
step S102, determining a first speed which is expected to be reached by the target object in a first preset duration according to a first preset transfer route, and determining a first position which is expected to be reached by the target object according to the first preset transfer route, the first speed and the first preset duration.
According to some alternative embodiments of the application, an influencing element for calculating the first speed is determined from the determined first preset transfer route, vehicle parameters, environmental data, wherein the influencing element is e.g. longitudinal grade, transverse grade, turning radius, viewing distance, longitudinal wind speed, transverse wind speed, wind direction, etc. And determining the weight of each influence element in calculating the first speed, and calculating the first speed which is expected to be reached by the target object in a first preset duration according to the first preset transfer route according to the plurality of influence elements and the weights corresponding to the influence elements one to one.
It can be appreciated that the first preset duration is a preset transfer duration, and the shorter the duration, the higher the accuracy of simulating the target object according to the first preset transfer route.
Alternatively, the target object is a mobile command post, such as an in-vehicle command post, where the command post is a place or facility for commanding, controlling and coordinating actions.
Step S104, determining whether the first position is in the coverage area of the optical satellite or not in the first target duration, and indicating the target object to execute the camouflage operation until the first position is not in the coverage area of the optical satellite in the second target duration under the condition that the first position is in the coverage area of the optical satellite in the first target duration, wherein the first target duration is the sum of the first preset duration and the duration required by the target object to execute the camouflage operation, and the second target duration is the sum of the first preset duration, the duration required by the target object to execute the camouflage operation and the duration required by the target object to release the camouflage operation.
According to other alternative embodiments of the present application, the first target time length is a first target period, a start time of transferring the target object according to the first preset transfer route is determined as a reference time, the reference time is set to be 0, the reference time is the start time of the first target period, and a time corresponding to a sum of the first preset time length and a time required for the target object to perform the camouflage operation is an end time of the first target period. The masquerading operations that can be performed by the command are, for example: with camouflage paint, reflective curtain wall, etc., it will be appreciated that the camouflage removal operation performed by the command will take a certain amount of time.
An optical satellite is an artificial satellite that observes the earth or other celestial body by mounting optical devices. Optical satellites primarily utilize optical systems to collect, record and transmit images and data of the earth or other celestial bodies. Optical satellites can provide high resolution images and data for research and applications in the fields of geological exploration, environmental monitoring, agriculture, urban planning, astronomy, etc. Optical satellites are typically equipped with a plurality of optical sensors, including optical cameras, spectrometers, lidars, and the like. The optical camera is used for shooting high-resolution color or black-and-white images, the spectrometer is used for analyzing the spectral characteristics of an object, and the laser radar is used for measuring the height information of the ground surface or the topography.
And step S106, when the first position is not in the coverage area of the optical satellite in the first target time period or when the first position is not in the coverage area of the optical satellite in the second target time period, the target object is instructed to move to the first position, and when the first position is coincident with the end point of the first preset transfer route, the target object is instructed to stop moving.
And if the first position is not in the coverage range of the optical satellite within a certain period of time, indicating the target object to move to the first position. If the first preset duration set in step S102 is required to be moved multiple times, for example, the second position, the third position and the fourth position are required to be passed to reach the end point of the first preset transfer route, the first preset transfer route is moved to the first position, and then the method indicated in step S102 to step S106 is repeatedly adopted to move to the second position, the third position and the fourth position until the first preset transfer route is reached.
According to the steps, the target object is instructed to move under the condition that the first position is not in the coverage area of the optical satellite in the first target duration or the first position is not in the coverage area of the optical satellite in the second target duration, so that the aim of reasonably controlling the target object to transfer is fulfilled, and the technical effect of improving the safety of the target object in the transfer process is achieved.
According to some alternative embodiments of the present application, determining whether the first location is within coverage of an electronic satellite for a first target period of time; under the condition that the first position is in the coverage area of the electronic satellite in the first target time length, indicating the target object to execute electromagnetic silencing operation until the first position is not in the coverage area of the electronic satellite in the first target time length, and recording the starting time and the ending time of the target object to execute the electromagnetic silencing operation; and determining the duration of the electromagnetic silence state of the target object in the first preset transfer line according to the starting time and the ending time.
Electromagnetic silencing refers to the use of specific electromagnetic technology means to reduce or completely eliminate electromagnetic radiation and electromagnetic signals generated by certain equipment or systems during operation, so as to achieve the purposes of reducing interference to surrounding environment and protecting equipment safety. Electromagnetic radiation refers to the energy carried by electromagnetic waves as they propagate in space, and common electromagnetic radiation includes radio waves, microwaves, infrared rays, visible light, ultraviolet rays, X-rays, gamma rays, and the like. Electromagnetic silencing techniques are implemented in a wide variety of ways, common methods including isolation shielding, spectrum control, radiation cancellation, radiation absorption, and the like. By means of reasonable design and optimization of equipment structure, adoption of special materials, use of filters, suppressors and the like, generation and propagation of electromagnetic radiation can be effectively reduced, and electromagnetic silencing effect is achieved.
An electronic satellite refers to a satellite vehicle that houses various electronic devices and instruments. The electronic equipment and the instrument can be used for various purposes such as communication, navigation, remote sensing, meteorological observation and the like. Communication satellites are one of the most common electronic satellites for providing communication services such as telephone, internet, and broadcast television worldwide. Navigation satellites are satellite systems used to provide accurate positioning and navigation services. Navigation satellites are typically equipped with a precision clock and receiver whose position can be determined by measuring the propagation time of the satellite signal. Remote sensing satellites are used to observe and monitor various natural and artificial phenomena on the earth's surface from space, equipped with various sensors, and capable of measuring information such as surface temperature, vegetation coverage, ocean surface temperature, atmospheric composition, etc. Meteorological satellites are used to observe and monitor various weather phenomena in the earth's atmosphere. The weather instrument is equipped, and can measure weather parameters such as cloud cover, temperature, humidity, wind speed and the like.
In some optional embodiments of the present application, after instructing the target object to perform the electromagnetic silencing operation until the first location is not within the coverage of the electronic satellite for the first target duration, the method further comprises: determining a first parameter according to the ratio of a first duration to a second duration, wherein the first duration is the duration of the target object in an electromagnetic silence state in a first preset transfer line, and the second duration is the duration of the target object from a starting point to an end point in the first preset transfer line; determining a second parameter according to the ratio of a third duration to a second duration, wherein the third duration is the duration of communication between the target object and other communicable objects in the first preset transfer line; determining a third parameter according to the ratio of the fourth duration to the second duration, wherein the fourth duration is the duration that the first value is larger than a preset threshold value in the first preset transfer line of the target object, and the first value is the ratio of the distance of communication between the target object and other communicable objects to the average height of the obstacle in the first preset transfer line; determining a first weight corresponding to the first parameter, a second weight corresponding to the second parameter and a third weight corresponding to the third parameter; and according to the first weight, the second weight and the third weight, carrying out weighted summation on the first parameter, the second parameter and the third parameter to obtain a target value, wherein the target value is used for representing the communication capacity of the target object in the first preset transfer line.
As some alternatives of the applicationIn the embodiment, the communication capacity in the preset transfer line is commanded, and several main factors of electromagnetic silence time, ultrashort wave communication, short wave communication and precipitation condition are considered. The electromagnetic silence is denoted as I 1 The weight coefficient is a 1 The method comprises the steps of carrying out a first treatment on the surface of the Ultrashort wave communication is marked as I 2 The weight coefficient is a 2 The method comprises the steps of carrying out a first treatment on the surface of the Short wave communication is denoted as I 3 The weight coefficient is a 3 The method comprises the steps of carrying out a first treatment on the surface of the The precipitation influence value is recorded as I 4 The weight coefficient is a 4 Wherein the weight coefficient a i The expert is given experience value according to actual situation.
The influence effect of each factor for determining the communication capability is divided into five gears of heavy influence, serious influence, moderate influence, slight influence and no influence, and each gear influence value is respectively 0, 0.25, 0.5, 0.75 and 1.
1. Electromagnetic silence time I 1 The influence gear division of the command station is determined by the duty ratio of a first time length in a second time length, wherein the first time length is the time length of the command station in a first preset transfer line in an electromagnetic silence state, and the second time length is the time length of the command station from a starting point to an end point in the first preset transfer line.
2. Ultrashort wave communication I 2 The influence gear division of the command is determined by the duty ratio of a third time length in a second time length, wherein the third time length is the time length of communication with other communicable objects in a first preset transfer line where the command is located.
3. Short wave communication I 3 The influence gear division of the command station is determined by the duty ratio of the fourth duration in the second duration, wherein the fourth duration is the duration that the first value is larger than a preset threshold value in the first preset transfer line where the command station is located, and the first value is the ratio of the distance of the command station for communicating with other communicable objects to the average height of the obstacle in the first preset transfer line.
4. Precipitation I 4 The influence gear of (2) is determined by the precipitation amount per unit time.
Obtaining a target value for representing the communication capacity of the preset transfer line where the command is located according to the following formula:
in some optional embodiments of the present application, scoring the preset transfer route at least according to the target value to obtain a scoring result; and displaying the scoring result corresponding to each preset transfer route in the plurality of preset transfer routes.
As further alternative embodiments of the present application, a second preset transfer route different from the first preset transfer route is acquired in the case where the first location is within the coverage of the optical satellite for a target preset time period; determining a second speed which is expected to be reached by the target object in a second preset time period according to a second preset transfer route, and determining a second position which is expected to be reached by the target object according to the second preset transfer route, the second speed and the second preset time period; determining whether the second position is in the coverage area of the optical satellite or not in a third target duration, and indicating the target object to execute camouflage operation until the second position is not in the coverage area of the optical satellite in a fourth target duration under the condition that the second position is in the coverage area of the optical satellite in the third target duration, wherein the third target duration is the sum of a second preset duration and a duration required by the target object to execute the camouflage operation, and the fourth target duration is the sum of the second preset duration, a duration required by the target object to execute the camouflage operation and a duration required by the target object to release the camouflage operation; and when the second position is not in the coverage range of the optical satellite in the third target duration or is not in the coverage range of the optical satellite in the fourth target duration, the target object is instructed to move to the second position, and when the second position is coincident with the end point of the second preset transfer route, the target object is instructed to stop moving.
Optionally, if the command is always within the coverage area of the optical satellite for a long period of time, selecting another transfer line different from the first preset transfer line, and indicating the command post to transfer according to the second preset transfer line.
In some alternative embodiments, determining a first speed that the target object is expected to reach within a first preset time period according to a first preset transfer route includes the steps of: acquiring a plurality of longitudinal gradients and a plurality of roll gradients in a first preset transfer route; determining a first average gradient value corresponding to the plurality of longitudinal gradients and a second average gradient value corresponding to the plurality of roll gradients; and determining the first speed at least according to the first average gradient value, the second average gradient value and the soil and pavement materials in the first preset transfer route.
First, factors affecting a first speed are determined, including soil and pavement material, longitudinal grade, roll grade, visibility, viewing distance, temperature, air pressure, humidity, lateral wind, longitudinal wind, precipitation, and vegetation. Secondly, the influence effects of all factors influencing communication are divided into five gears of bad influence, serious influence, moderate influence, slight influence and no influence, and each gear influence value is 0, 0.25, 0.5, 0.75 and 1 respectively. The expert or other mode gives the value range of each gear of each influencing factor, and then gives the influencing value I after determining the gear according to the actual value 1 -I 12 . Finally, according to the weight parameter a determined by expert 1 -a 12 And an influence value I 1 -I 12 Calculating the influence coefficient of the environmental factors of each point on the first preset transfer route on the theoretical maximum speedFurther, the point speed is determined>Wherein V is 0 The maximum speed of the corresponding vehicle is commanded, and is a fixed value related to the vehicle model.
According to some preferred embodiments of the application, the method further comprises, before determining whether the first location is within the coverage area of the optical satellite for a first target period of time: determining the distance from the optical satellite to the earth center according to the semi-long axis of the optical satellite; determining the true near point angle of the optical satellite according to the eccentricity of the optical satellite; determining a first coordinate of the optical satellite in a satellite orbit coordinate system according to the distance from the optical satellite to the earth center and the true near point angle; converting the first coordinate into a geodetic coordinate system, and obtaining longitude and latitude corresponding to the optical satellite in the geodetic coordinate system; determining the projection position of the optical satellite on the ground according to the longitude and latitude corresponding to the optical satellite; and determining the coverage range of the optical satellite according to the projection position of the optical satellite on the ground and the coverage radius of the optical satellite.
According to some alternative embodiments of the present application, a two-body model of satellite orbits is determined using six orbits, wherein the six orbits include: semi-long axis a, eccentricity e, track inclination i, near-spot amplitude The ascending intersection is right through->True near point angle->Six parameters.
Specifically, an orbital coordinate system is first established, the origin of coordinates of the coordinate system being located at the earth's center,，/>the axis being located on the plane of the track,/->Normal vector of axis and orbit plane +.>And overlapping, wherein the orbit coordinate system is a right-hand coordinate system.
The average angle M is calculated by
Wherein t is 0 The moment when the satellite is too close to the spot, n is the average angular velocity of the satellite, where,
wherein a is a semi-long axis of the track, G is a constant of gravitational force, M e Is the earth radius.
Solving the Prussian equation, and calculating a near point angle E:。
calculating the distance r from the satellite to the earth center:
calculating true near point angle：
Calculating coordinates of satellites in an orbital coordinate system:
the orbit coordinate is converted into the geodetic coordinate system, and the orbit coordinate system can be rotated for three times to be matched with the geodetic space rectangular coordinate systemAnd (3) superposition: first wind->The shaft rotates anticlockwise +.>Angle, make->Rotate to->(point to the rising intersection point); second, wind->Rotate counter-clockwise by an angle i, thus +.>And->Overlapping; finally wind->Counterclockwise rotation->The two coordinate systems are brought into coincidence, wherein +.>Is->Axle and spring point->The angle of the directions (greenwich fixed star time angle).
Then, there are:
the geocentric coordinate system is converted into a geographic longitude and latitude coordinate system by longitude and latitude and geodetic altitude To indicate the location of the point. The conversion mode is as follows:
wherein L, B is the longitude and latitude of the satellite.
Finally, the satellite coverage is determined by the projection position of the satellite on the ground surface and the coverage radius, the satellite projection position can be obtained according to the longitude and latitude L, B of the satellite, and then the coverage can be calculated according to the coverage radius.
Fig. 2 is a flowchart of another method for transferring a target object according to an embodiment of the present application, as shown in fig. 2, the method includes the steps of:
step S201, recording the current position of the command post asThe current time is recorded as->Optionally, the current timeThe analog time interval (first preset duration) is noted +.>The time period required for performing the disguise operation is marked +.>The time period required for the disguise operation to be removed is marked +.>。
Step S202, starting from the starting point, the command post at the current positionSet as the starting point +.>The command post action state is set to "move", and the electromagnetic silence state is set to "not silence".
Step S203, if the command post state is "move", continuing. If the director status is "execute camouflage", the process goes to step S210. If the command post status is "disguise," go to step S211. If the command post status is: "complete camouflage", turning to step S212, FIG. 3 is a schematic diagram of a command post action state according to an embodiment of the application.
Step S204, calculating the current position according to the maneuvering model and the geographical topography and meteorological hydrologic data at the starting pointMotor speed which can be reached by command post at the place +.>。
Step S205, calculating the speedElapsed time->Afterwards, the command can reach the position +.>
Until the command post has reached the endpoint.
Step S206, calculating the time in time according to the optical satellite orbit dataCoverage of optical satellite ∈>。
Step S207, judgingWhether or not in the coverage area of an optical satellite->And (3) inner part. If the determination result is that the optical satellite is within the coverage area, the process goes to step S209, and if the determination result is that the optical satellite is not within the coverage area, the process goes to step S208.
Step S208, the command post continues to move, the current positionSet to->Go to step S215.
In step S209, the command post stops moving, the status is set to "execute masquerading", the action timer is set to the time required to execute masquerading, and the process goes to step S214.
Step S210, the command post continues to execute camouflage, and the action timer is reducedIs a time of (a) to be used. If the remaining time is 0 or less, the director state is set to "complete camouflage", and the process goes to step S214.
Step S211, the command post continues to remove disguise, and the action timer is reduced Is a time of (a) to be used. If the remaining time is 0 or less, the director state is set to "move", and the process goes to step S214.
Step S212, calculating the coverage of the optical satellite at the current momentIf the command post can be covered, continuing to keep camouflage, and turning to step S214; if not covered, step S213 is continued.
Step S213, calculateTo->During which the optical satellite coverage is high,，/>if neither of the periods is observed, the disguise is started, the command post action state is set to "disguise", the action timer is set to the time required to perform disguise, and the process proceeds to step S214.
The time is used hereBecause enough re-disguise time needs to be reserved to avoid detecting satellites soon after disguise has been removed, resulting in insufficient time for re-disguising.
Step S214, calculating time from the electronic satellite orbit dataAll electronic satellite coverage ∈ ->。
Step S215, judgeWhether or not in the coverage of an electronic satellite->In the method, if the judgment result is that the electromagnetic silence state of the command post is in the coverage area of the electronic satellite, the electromagnetic silence state of the command post is set to be 'silence', and if the judgment result is that the electromagnetic silence state of the command post is not in the coverage area of the electronic satellite, the electromagnetic silence state of the command post is set to be 'not silence'.
Step S216, calculating the current command communication capacity of the command post according to the geographical topography, the meteorological hydrologic data and the silence condition.
Step S217, if the command post reaches the end point, the simulation is ended, otherwise, the simulation is continued.
Step S218, the current timeChange to->Returning to step S203, the simulation at the next time point is performed.
Fig. 4 is a block diagram of a transfer apparatus of a target object according to an embodiment of the present application, as shown in fig. 4, the apparatus including:
a first determining module 40, configured to determine a first speed that the target object is expected to reach in a first preset duration according to a first preset transfer route, and determine a first position that the target object is expected to reach according to the first preset transfer route, the first speed, and the first preset duration;
a first control module 42, configured to determine whether the first position is within a coverage area of the optical satellite within a first target duration, and instruct the target object to perform the camouflage operation when the first position is within the coverage area of the optical satellite within the first target duration until the first position is not within the coverage area of the optical satellite within a second target duration, where the first target duration is a sum of a first preset duration and a duration required by the target object to perform the camouflage operation, and the second target duration is a sum of the first preset duration, a duration required by the target object to perform the camouflage operation, and a duration required by the target object to release the camouflage operation;
The second control module 44 is configured to instruct the target object to move to the first position when the first position is not within the coverage area of the optical satellite within the first target duration, or instruct the target object to stop moving when the first position is coincident with the end point of the first preset transfer route when the first position is not within the coverage area of the optical satellite within the second target duration.
Note that each module in fig. 4 may be a program module (for example, a set of program instructions for implementing a specific function), or may be a hardware module, and for the latter, it may be represented by the following form, but is not limited thereto: the expression forms of the modules are all a processor, or the functions of the modules are realized by one processor.
It should be noted that, the preferred implementation manner of the embodiment shown in fig. 4 may refer to the related description of the embodiment shown in fig. 1, which is not repeated herein.
Optionally, determining whether the first location is within a coverage area of the electronic satellite for a first target duration; under the condition that the first position is in the coverage area of the electronic satellite in the first target time length, indicating the target object to execute electromagnetic silencing operation until the first position is not in the coverage area of the electronic satellite in the first target time length, and recording the starting time and the ending time of the target object to execute the electromagnetic silencing operation; and determining the duration of the electromagnetic silence state of the target object in the first preset transfer line according to the starting time and the ending time.
Optionally, after instructing the target object to perform the electromagnetic silencing operation until the first position is not within the coverage of the electronic satellite for the first target duration, the method further includes: determining a first parameter according to the ratio of a first duration to a second duration, wherein the first duration is the duration of the target object in an electromagnetic silence state in a first preset transfer line, and the second duration is the duration of the target object from a starting point to an end point in the first preset transfer line; determining a second parameter according to the ratio of a third duration to a second duration, wherein the third duration is the duration of communication between the target object and other communicable objects in the first preset transfer line; determining a third parameter according to the ratio of the fourth duration to the second duration, wherein the fourth duration is the duration that the first value is larger than a preset threshold value in the first preset transfer line of the target object, and the first value is the ratio of the distance of communication between the target object and other communicable objects to the average height of the obstacle in the first preset transfer line; determining a first weight corresponding to the first parameter, a second weight corresponding to the second parameter and a third weight corresponding to the third parameter; and according to the first weight, the second weight and the third weight, carrying out weighted summation on the first parameter, the second parameter and the third parameter to obtain a target value, wherein the target value is used for representing the communication capacity of the target object in the first preset transfer line.
Optionally, scoring the preset transfer route at least according to the target value to obtain a scoring result; and displaying the scoring result corresponding to each preset transfer route in the plurality of preset transfer routes.
Optionally, acquiring a second preset transfer route different from the first preset transfer route under the condition that the first position is within the coverage range of the optical satellite within the target preset time period; determining a second speed which is expected to be reached by the target object in a second preset time period according to a second preset transfer route, and determining a second position which is expected to be reached by the target object according to the second preset transfer route, the second speed and the second preset time period; determining whether the second position is in the coverage area of the optical satellite or not in a third target duration, and indicating the target object to execute camouflage operation until the second position is not in the coverage area of the optical satellite in a fourth target duration under the condition that the second position is in the coverage area of the optical satellite in the third target duration, wherein the third target duration is the sum of a second preset duration and a duration required by the target object to execute the camouflage operation, and the fourth target duration is the sum of the second preset duration, a duration required by the target object to execute the camouflage operation and a duration required by the target object to release the camouflage operation; and when the second position is not in the coverage range of the optical satellite in the third target duration or is not in the coverage range of the optical satellite in the fourth target duration, the target object is instructed to move to the second position, and when the second position is coincident with the end point of the second preset transfer route, the target object is instructed to stop moving.
Optionally, determining the first speed that the target object is expected to reach in the first preset duration according to the first preset transfer route includes: acquiring a plurality of longitudinal gradients and a plurality of roll gradients in a first preset transfer route; determining a first average gradient value corresponding to the plurality of longitudinal gradients and a second average gradient value corresponding to the plurality of roll gradients; and determining the first speed at least according to the first average gradient value, the second average gradient value and the soil and pavement materials in the first preset transfer route.
Optionally, before determining whether the first location is within the coverage of the optical satellite for the first target duration, the method further comprises: determining the distance from the optical satellite to the earth center according to the semi-long axis of the optical satellite; determining the true near point angle of the optical satellite according to the eccentricity of the optical satellite; determining a first coordinate of the optical satellite in a satellite orbit coordinate system according to the distance from the optical satellite to the earth center and the true near point angle; converting the first coordinate into a geodetic coordinate system, and obtaining longitude and latitude corresponding to the optical satellite in the geodetic coordinate system; determining the projection position of the optical satellite on the ground according to the longitude and latitude corresponding to the optical satellite; and determining the coverage range of the optical satellite according to the projection position of the optical satellite on the ground and the coverage radius of the optical satellite.
Fig. 5 shows a hardware block diagram of a computer terminal (or mobile device) for implementing a transfer method of a target object. As shown in fig. 5, the computer terminal 50 (or mobile device 50) may include one or more processors 502 (shown in the figures as 502a, 502b, … …,502 n) (the processor 502 may include, but is not limited to, a microprocessor MCU, a programmable logic device FPGA, etc.) a memory 504 for storing data, and a transmission module 506 for communication functions. In addition, the method may further include: a display, an input/output interface (I/O interface), a Universal Serial BUS (USB) port (which may be included as one of the ports of the BUS), a network interface, a power supply, and/or a camera. It will be appreciated by those of ordinary skill in the art that the configuration shown in fig. 5 is merely illustrative and is not intended to limit the configuration of the electronic device described above. For example, the computer terminal 50 may also include more or fewer components than shown in FIG. 5, or have a different configuration than shown in FIG. 5.
It should be noted that the one or more processors 502 and/or other data processing circuits described above may be referred to herein generally as "data processing circuits. The data processing circuit may be embodied in whole or in part in software, hardware, firmware, or any other combination. Furthermore, the data processing circuitry may be a single stand-alone processing module, or incorporated, in whole or in part, into any of the other elements in the computer terminal 50 (or mobile device). As referred to in embodiments of the application, the data processing circuit acts as a processor control (e.g., selection of the path of the variable resistor termination connected to the interface).
The memory 504 may be used to store software programs and modules of application software, such as program instructions/data storage devices corresponding to the method for transferring a target object in the embodiment of the present application, and the processor 502 executes the software programs and modules stored in the memory 504, thereby performing various functional applications and data processing, that is, implementing the method for transferring a target object. Memory 504 may include high-speed random access memory, and may also include non-volatile memory, such as one or more magnetic storage devices, flash memory, or other non-volatile solid-state memory. In some examples, the memory 504 may further comprise memory located remotely from the processor 502, which may be connected to the computer terminal 50 via a network. Examples of such networks include, but are not limited to, the internet, intranets, local area networks, mobile communication networks, and combinations thereof.
The transmission module 506 is used to receive or transmit data via a network. The specific examples of the network described above may include a wireless network provided by a communication provider of the computer terminal 50. In one example, the transmission module 506 includes a network adapter (Network Interface Controller, NIC) that can connect to other network devices through a base station to communicate with the internet. In one example, the transmission module 506 may be a Radio Frequency (RF) module, which is used to communicate with the internet wirelessly.
The display may be, for example, a touch screen type Liquid Crystal Display (LCD) that may enable a user to interact with a user interface of the computer terminal 50 (or mobile device).
It should be noted here that, in some alternative embodiments, the computer device (or the electronic device) shown in fig. 5 may include hardware elements (including circuits), software elements (including computer code stored on a computer readable medium), or a combination of both hardware elements and software elements. It should be noted that fig. 5 is only one example of a specific example, and is intended to illustrate the types of components that may be present in the computer device (or electronic device) described above.
It should be noted that, the electronic device shown in fig. 5 is used for executing the transferring method of the target object shown in fig. 1, so the explanation related to the executing method of the command is also applicable to the electronic device, and will not be repeated here.
The embodiment of the application also provides a nonvolatile storage medium, which comprises a stored program, wherein the program controls the equipment where the storage medium is located to execute the above target object transferring method when running.
The nonvolatile storage medium executes a program of the following functions: determining a first speed which is expected to be reached by the target object in a first preset duration according to a first preset transfer route, and determining a first position which is expected to be reached by the target object according to the first preset transfer route, the first speed and the first preset duration; determining whether the first position is in the coverage area of the optical satellite or not in a first target duration, and indicating the target object to execute camouflage operation until the first position is not in the coverage area of the optical satellite in a second target duration under the condition that the first position is in the coverage area of the optical satellite in the first target duration, wherein the first target duration is the sum of a first preset duration and a duration required by the target object to execute the camouflage operation, and the second target duration is the sum of the first preset duration, a duration required by the target object to execute the camouflage operation and a duration required by the target object to release the camouflage operation; and when the first position is not in the coverage range of the optical satellite in the first target duration or is not in the coverage range of the optical satellite in the second target duration, the target object is instructed to move to the first position, and when the first position is coincident with the end point of the first preset transfer route, the target object is instructed to stop moving.
The embodiment of the application also provides electronic equipment, which comprises: the system comprises a memory and a processor, wherein the processor is used for running a program stored in the memory, and the program runs to execute the transfer method of the target object.
The processor is configured to execute a program that performs the following functions: determining a first speed which is expected to be reached by the target object in a first preset duration according to a first preset transfer route, and determining a first position which is expected to be reached by the target object according to the first preset transfer route, the first speed and the first preset duration; determining whether the first position is in the coverage area of the optical satellite or not in a first target duration, and indicating the target object to execute camouflage operation until the first position is not in the coverage area of the optical satellite in a second target duration under the condition that the first position is in the coverage area of the optical satellite in the first target duration, wherein the first target duration is the sum of a first preset duration and a duration required by the target object to execute the camouflage operation, and the second target duration is the sum of the first preset duration, a duration required by the target object to execute the camouflage operation and a duration required by the target object to release the camouflage operation; and when the first position is not in the coverage range of the optical satellite in the first target duration or is not in the coverage range of the optical satellite in the second target duration, the target object is instructed to move to the first position, and when the first position is coincident with the end point of the first preset transfer route, the target object is instructed to stop moving.
The foregoing embodiment numbers of the present application are merely for the purpose of description, and do not represent the advantages or disadvantages of the embodiments.
In the foregoing embodiments of the present application, the descriptions of the embodiments are emphasized, and for a portion of this disclosure that is not described in detail in this embodiment, reference is made to the related descriptions of other embodiments.
In the several embodiments provided in the present application, it should be understood that the disclosed technology may be implemented in other manners. The above-described embodiments of the apparatus are merely exemplary, and the division of the units, for example, may be a logic function division, and may be implemented in another manner, for example, a plurality of units or components may be combined or may be integrated into another system, or some features may be omitted, or not performed. Alternatively, the coupling or direct coupling or communication connection shown or discussed with each other may be through some interfaces, units or modules, or may be in electrical or other forms.
The units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.
In addition, each functional unit in the embodiments of the present application may be integrated in one processing unit, or each unit may exist alone physically, or two or more units may be integrated in one unit. The integrated units may be implemented in hardware or in software functional units.
The integrated units, if implemented in the form of software functional units and sold or used as stand-alone products, may be stored in a computer readable storage medium. Based on such understanding, the technical solution of the present application may be embodied in essence or a part contributing to the related art or all or part of the technical solution, in the form of a software product stored in a storage medium, including several instructions for causing a computer device (which may be a personal computer, a server or a network device, etc.) to perform all or part of the steps of the method according to the embodiments of the present application. And the aforementioned storage medium includes: a U-disk, a Read-Only Memory (ROM), a random access Memory (RAM, random Access Memory), a removable hard disk, a magnetic disk, or an optical disk, or other various media capable of storing program codes.
The foregoing is merely a preferred embodiment of the present application and it should be noted that modifications and adaptations to those skilled in the art may be made without departing from the principles of the present application, which are intended to be comprehended within the scope of the present application.

Claims (10)

1. A method of transferring a target object, comprising:
determining a first speed which is expected to be reached by a target object in a first preset duration according to a first preset transfer route, and determining a first position which is expected to be reached by the target object according to the first preset transfer route, the first speed and the first preset duration;
determining whether the first position is in the coverage area of an optical satellite or not in a first target duration, and indicating the target object to execute camouflage operation until the first position is not in the coverage area of the optical satellite in a second target duration under the condition that the first position is in the coverage area of the optical satellite in the first target duration, wherein the first target duration is the sum of the first preset duration and the duration required by the target object to execute the camouflage operation, and the second target duration is the sum of the first preset duration, the duration required by the target object to execute the camouflage operation and the duration required by the target object to release the camouflage operation;
And when the first position is not in the coverage range of the optical satellite in the first target duration or is not in the coverage range of the optical satellite in the second target duration, the target object is indicated to move to the first position, and when the first position is coincident with the end point of the first preset transfer route, the target object is indicated to stop moving.
2. The method according to claim 1, characterized in that it comprises:
determining whether the first location is within a coverage area of an electronic satellite within the first target duration;
under the condition that the first position is in the coverage range of the electronic satellite in the first target duration, the target object is instructed to execute electromagnetic silencing operation until the first position is not in the coverage range of the electronic satellite in the first target duration, and the starting time and the ending time of the target object to execute the electromagnetic silencing operation are recorded;
and determining the duration of the target object in the electromagnetic silence state in the first preset transfer route according to the starting time and the ending time.
3. The method of claim 2, wherein the target object is instructed to perform an electromagnetic silencing operation until after the first location is not within coverage of the electronic satellite for the first target duration, the method further comprising:
determining a first parameter according to the ratio of a first duration to a second duration, wherein the first duration is the duration of the target object in the electromagnetic silence state in the first preset transfer route, and the second duration is the duration of the target object from a starting point to an ending point in the first preset transfer route;
determining a second parameter according to the ratio of a third duration to the second duration, wherein the third duration is the duration of communication between the target object and other communicable objects in the first preset transfer route;
determining a third parameter according to the ratio of a fourth duration to the second duration, wherein the fourth duration is the duration that a first value is greater than a preset threshold value in the first preset transfer route of the target object, and the first value is the ratio of the distance that the target object communicates with the other communicable objects to the average height of the obstacle in the first preset transfer route;
Determining a first weight corresponding to the first parameter, a second weight corresponding to the second parameter and a third weight corresponding to a third parameter;
and carrying out weighted summation on the first parameter, the second parameter and the third parameter according to the first weight, the second weight and the third weight to obtain a target value, wherein the target value is used for representing the communication capacity of the target object in the first preset transfer route.
4. A method according to claim 3, comprising:
scoring the first preset transfer route at least according to the target value to obtain a scoring result;
and displaying the scoring result corresponding to each of the first preset transfer routes in the plurality of first preset transfer routes.
5. The method according to claim 1, wherein the method further comprises:
acquiring a second preset transfer route different from the first preset transfer route under the condition that the first position is within the coverage range of the optical satellite within a target preset time length;
determining a second speed which is expected to be reached by the target object in a second preset time period according to the second preset transfer route, and determining a second position which is expected to be reached by the target object according to the second preset transfer route, the second speed and the second preset time period;
Determining whether the second position is in the coverage area of the optical satellite in a third target duration, and indicating the target object to execute camouflage operation until the second position is not in the coverage area of the optical satellite in a fourth target duration, wherein the third target duration is the sum of the second preset duration and the duration required by the target object to execute the camouflage operation, and the fourth target duration is the sum of the second preset duration, the duration required by the target object to execute the camouflage operation and the duration required by the target object to release the camouflage operation;
and when the second position is not in the coverage range of the optical satellite in the third target duration or is not in the coverage range of the optical satellite in the fourth target duration, the target object is instructed to move to the second position, and when the second position is coincident with the end point of the second preset transfer route, the target object is instructed to stop moving.
6. The method of claim 1, wherein determining a first speed that the target object is expected to reach for a first predetermined duration according to a first predetermined transfer route comprises:
acquiring a plurality of longitudinal gradients and a plurality of roll gradients in the first preset transfer route;
determining a first average slope value corresponding to the plurality of longitudinal slopes and a second average slope value corresponding to the plurality of roll slopes;
and determining the first speed at least according to the first average gradient value, the second average gradient value and the soil and pavement materials in the first preset transfer route.
7. The method of claim 1, wherein determining whether the first location is within a coverage area of an optical satellite for a first target time period is preceded by:
determining the distance from the optical satellite to the earth center according to the semi-long axis of the optical satellite;
determining a true near point angle of the optical satellite according to the eccentricity of the optical satellite;
determining a first coordinate of the optical satellite in a satellite orbit coordinate system according to the distance from the optical satellite to the earth center and the true near point angle;
Converting the first coordinate into a geodetic coordinate system, and obtaining the longitude and latitude corresponding to the optical satellite in the geodetic coordinate system;
determining the projection position of the optical satellite on the ground according to the longitude and latitude corresponding to the optical satellite;
and determining the coverage range of the optical satellite according to the projection position of the optical satellite on the ground and the coverage radius of the optical satellite.
8. A transfer apparatus for a target object, comprising:
the first determining module is used for determining a first speed which is expected to be reached by the target object in a first preset duration according to a first preset transfer route, and determining a first position which is expected to be reached by the target object according to the first preset transfer route, the first speed and the first preset duration;
a first control module, configured to determine whether the first position is within a coverage area of an optical satellite within a first target duration, and instruct the target object to perform a masquerading operation when the first position is within the coverage area of the optical satellite within the first target duration, until the first position is not within the coverage area of the optical satellite within a second target duration, where the first target duration is a sum of the first preset duration and a duration required by the target object to perform the masquerading operation, and the second target duration is a sum of the first preset duration, a duration required by the target object to perform the masquerading operation, and a duration required by the target object to release the masquerading operation;
And the second control module is used for indicating the target object to move to the first position when the first position is not in the coverage range of the optical satellite in the first target duration or not in the coverage range of the optical satellite in the second target duration, and indicating the target object to stop moving when the first position is coincident with the end point of the first preset transfer route.
9. A non-volatile storage medium, characterized in that the non-volatile storage medium comprises a stored program, wherein the program, when run, controls a device in which the non-volatile storage medium is located to perform the transfer method of the target object according to any one of claims 1 to 7.
10. An electronic device, comprising: a memory and a processor for executing a program stored in the memory, wherein the program is executed to perform the transfer method of the target object according to any one of claims 1 to 7.
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