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CN-122001435-A - Method and device for guiding star by terminal, terminal and readable storage medium

CN122001435ACN 122001435 ACN122001435 ACN 122001435ACN-122001435-A

Abstract

The application provides a method and a device for guiding a star by a terminal, the terminal and a readable storage medium, and relates to the technical field of terminals. The method includes the steps of displaying first indication information in response to operation of opening a first application in a satellite communication mode, wherein the first indication information is used for indicating the relative position between a communication satellite and a first radiation range of a satellite antenna, the first radiation range is related to signal quality required by the first application, displaying second indication information in response to operation of opening a second application, the second indication information is used for indicating the relative position between the communication satellite and a second radiation range of the satellite antenna, the second radiation range is related to signal quality required by the second application, the first radiation angle of the first radiation range is different from the second radiation angle of the second radiation range, and based on the first indication information, a terminal is guided to adjust the direction of the terminal through indication information corresponding to different satellite applications, and accordingly the signal quality of the terminal meets the signal quality required by the satellite application in operation.

Inventors

  • ZHANG YUNJI

Assignees

  • 华为终端有限公司

Dates

Publication Date
20260508
Application Date
20241105

Claims (14)

  1. 1. A method for guiding a satellite by a terminal, which is applied to the terminal, wherein a satellite antenna is arranged in the terminal, the method comprises the following steps: In a satellite communication mode, in response to an operation of opening a first application, displaying first indication information, wherein the first indication information is used for indicating the relative position between a communication satellite and a first radiation range of the satellite antenna, and the first radiation range is related to signal quality required by the first application when running; And in response to an operation of opening a second application, displaying second indication information, wherein the second indication information is used for indicating the relative position between a communication satellite and a second radiation range of the satellite antenna, the second radiation range is related to signal quality required by the second application in operation, and a first radiation angle corresponding to the first radiation range is different from a second radiation angle corresponding to the second radiation range.
  2. 2. The method according to claim 1, wherein the method further comprises: And under the condition that the radiation range is not aligned with the communication satellite, displaying first guiding information, wherein the first guiding information is used for guiding a user to adjust the direction of the terminal so as to align the radiation range with the communication satellite, and the radiation range is the first radiation range or the second radiation range.
  3. 3. The method of claim 2, wherein the first guidance information is icon information or text information.
  4. 4. A method according to any of claims 1-3, characterized in that the second radiation angle is smaller than the first radiation angle in case the signal quality required at the time of operation of the second application is larger than the signal quality required at the time of operation of the first application; The second radiation angle is larger than the first radiation angle in case the signal quality required by the second application when running is smaller than the signal quality required by the first application when running.
  5. 5. The method of any one of claims 1 to 4, wherein the first indication information comprises a satellite identification and a first radiation pattern, the first radiation pattern being used to indicate the first radiation range, the satellite identification being used to indicate the communication satellite; the second indication information includes the satellite identification and a second radiation pattern for indicating the second radiation range.
  6. 6. The method of claim 5, wherein the operation of opening the second application is an operation of switching the first application to the second application; in the case that the second radiation angle is smaller than the first radiation angle, the second indication information further includes the first radiation pattern, and the first radiation pattern is different from the second radiation pattern in color.
  7. 7. The method of any one of claims 1 to 4, wherein the indication information comprises a first pattern or a second pattern, the first pattern and the second pattern being different in color or shape, the first pattern being for indicating that a radiation range of the satellite antenna is aligned with the communication satellite, the second pattern being for indicating that the radiation range is not aligned with the communication satellite; The radiation range is the first radiation range when the indication information is the first indication information, and the radiation range is the second radiation range when the indication information is the second indication information.
  8. 8. The method according to any one of claims 1 to 7, wherein the first indication information and/or the second indication information comprises a textual indication information.
  9. 9. The method according to any one of claims 1 to 8, further comprising: In the process of displaying the indication information, responding to the operation of switching the terminal from the current folding state to the unfolding state, displaying third indication information, wherein the third indication information is used for indicating the relative position between the communication satellite and a third radiation range of the satellite antenna when the terminal is in the unfolding state, and a third radiation angle corresponding to the third radiation range is larger than a radiation angle corresponding to the radiation range of the satellite antenna; The radiation range is the first radiation range, the radiation angle is the first radiation angle, and the radiation range is the second radiation range, the radiation angle is the second radiation angle, the indication information is the second indication information.
  10. 10. The method according to any one of claims 1 to 8, further comprising: In the process of displaying the indication information, responding to the operation of switching the terminal from the current unfolding state to the folding state, displaying fourth indication information, wherein the fourth indication information is used for indicating the relative position between the communication satellite and a fourth radiation range of the satellite antenna when the terminal is in the folding state, and a fourth radiation angle corresponding to the fourth radiation range is larger than a radiation angle corresponding to the radiation range of the satellite antenna; The radiation range is the first radiation range, the radiation angle is the first radiation angle, and the radiation range is the second radiation range, the radiation angle is the second radiation angle, the indication information is the second indication information.
  11. 11. A terminal-to-star guiding device, characterized by comprising at least one unit for implementing the method according to any one of claims 1 to 10.
  12. 12. A terminal comprising a processor for running a computer program stored in a memory to implement the method of any one of claims 1 to 10.
  13. 13. A computer readable storage medium, characterized in that the computer readable storage medium stores a computer program which, when executed by a computer, implements the method according to any one of claims 1 to 10.
  14. 14. A computer program product comprising computer program code which, when executed by a computer, implements the method of any of claims 1 to 10.

Description

Method and device for guiding star by terminal, terminal and readable storage medium Technical Field The present application relates to the field of terminal technologies, and in particular, to a method and apparatus for guiding a star by a terminal, and a readable storage medium. Background Satellite communication is not easily affected by geographical environment, so that communication satellites can provide communication services for terminals with satellite communication functions in areas which cannot be covered by cellular networks such as oceans, deserts, unmanned areas and the like. After a general user starts a satellite communication mode of the terminal, the terminal can communicate with a communication satellite through a satellite antenna in the device. Specifically, the terminal can display the relative position relationship between the current communication satellite and the terminal in the display interface according to the ephemeris of the communication satellite, and the user can enable the communication satellite to be located in the signal radiation range of the satellite antenna by adjusting the direction of the terminal, so that satellite communication connection is established between the terminal and the communication satellite. The signal radiation intensity of the satellite antenna is different in different directions, so that when the communication satellite is located in different directions of the satellite antenna, the signal quality between the terminal and the communication satellite is also different. Based on this, when the communication satellite is located in a certain direction within the signal radiation range of the satellite antenna, the signal quality of the terminal may be too low, so that the signal quality cannot meet the service requirements of part of the application software. Disclosure of Invention The application provides a satellite communication method, a satellite communication device, a terminal and a readable storage medium, which can solve the technical problem that partial applications in the terminal cannot be used due to lower signal quality between the terminal and a satellite. In order to achieve the above purpose, the application adopts the following technical scheme: in a first aspect, the application provides a method for guiding a satellite by a terminal, which is applied to the terminal provided with a satellite antenna, and the method specifically comprises the steps of responding to an operation of opening a first application in a satellite communication mode, displaying first indication information, wherein the first indication information is used for indicating the relative position between a communication satellite and a first radiation range of the satellite antenna, the first radiation range is related to signal quality required by the first application in operation, responding to an operation of opening a second application, displaying second indication information, the second indication information is used for indicating the relative position between the communication satellite and a second radiation range of the satellite antenna, the second radiation range is related to signal quality required by the second application in operation, and a first radiation angle corresponding to the first radiation range is different from a second radiation angle corresponding to the second radiation range. By way of example, signal quality may be expressed in terms of signal strength (SIGNAL STRENGTH), signal-to-noise ratio (signal to noise ratio, SNR), or other parameters. The signal quality required for each application to run may be the minimum signal quality required for implementing the application functions of the application itself, e.g. the minimum signal strength or the minimum signal to noise ratio. Further, if a certain application has multiple application functions and the signal quality required for implementing different application functions is different, the signal quality required for running the application may be an average signal quality required for implementing multiple application functions of the application, where the value of the average signal quality may be an average value of parameters corresponding to the signal quality required for implementing different application functions of the application. In the guiding method provided by the embodiment of the application, when the terminal is in the satellite communication mode, after a user opens different applications in the terminal, the terminal can display different indication information according to the radiation range of the satellite antenna corresponding to the information quality required by each application in operation and the ephemeris of the communication satellite, so as to display the relative position relation between the communication satellite and the radiation range corresponding to the currently opened application to the user, and further prompt the user w