WO2019165730A1 - 模拟星球登陆的教学方法以及装置 - Google Patents

模拟星球登陆的教学方法以及装置 Download PDF

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Publication number
WO2019165730A1
WO2019165730A1 PCT/CN2018/092771 CN2018092771W WO2019165730A1 WO 2019165730 A1 WO2019165730 A1 WO 2019165730A1 CN 2018092771 W CN2018092771 W CN 2018092771W WO 2019165730 A1 WO2019165730 A1 WO 2019165730A1
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WIPO (PCT)
Prior art keywords
spacecraft
information
landing
user
orbit
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PCT/CN2018/092771
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English (en)
French (fr)
Inventor
卢启伟
刘善果
刘胜强
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深圳市鹰硕技术有限公司
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Publication of WO2019165730A1 publication Critical patent/WO2019165730A1/zh

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    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q50/00—Information and communication technology [ICT] specially adapted for implementation of business processes of specific business sectors, e.g. utilities or tourism
    • G06Q50/10—Services
    • G06Q50/20—Education
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/24—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer including display or recording of simulated flight path

Definitions

  • the present disclosure relates to the field of computer technology, and in particular, to a teaching method, apparatus, electronic device, and computer readable storage medium for simulating a planetary landing.
  • Patent Application No. CN201710159287.6 discloses a simulated space capsule system for adolescent defense aerospace education, and discloses the infrastructure in the system, including space capsules, bulkhead pads, inner cabin floors, escape cabins, Left-hand propellers, right-hand propellers, intake hatches, intake switch rotary handles, etc., aim to use the simulated space capsule system to demonstrate aerospace culture and aerospace technology to create a realistic space simulation environment that allows young people to pass simulations.
  • Space facilities and space capsule environments experience the space-free life of a space-free state and a reversing maneuver.
  • This application only discloses a hardware facility for a simulated space capsule system dedicated to aerospace education. It can only provide adolescents with a microgravity sensory experience for the space environment, and cannot provide the user with the teaching purpose of the planet landing process.
  • the patent application with the application number CN201210484568.6 discloses a spatial microgravity simulation experiment system, which mainly comprises a peripheral frame, a leveling system, a passive adjustment mechanism in a horizontal plane, a Z-direction active gravity compensation system, a rotary passive adjustment mechanism, and a pitch deflection active. Adjust the system, and simulate the space microgravity environment through the cooperation between the components, complete the change of the posture of the experimental object, and reproduce the zero gravity state.
  • the patent application with the application number CN03276220.8 discloses a simulated spacecraft, which is controlled centrally by computer, according to the progress of the aerospace, the "outside window" scene played by the television, the sound, the collision, the vibration, and the flight position with the utility model.
  • the flight angle of 2 and the temperature in the warehouse are consistent, which makes visitors feel the experience of space flight realistically, and feel a variety of space movements such as tilting, turning, collision, shaking, and rotation.
  • Application No. CN00234436.X is a magnetic levitation space amusement ship.
  • the high-strength magnet on the bottom of the ship and the high-strength magnet on the running slide are used to suspend the amusement boat.
  • the space invites. The feeling of swimming.
  • the present disclosure is directed to the above problems existing in the prior art, mainly for enabling a user to perform a space experience in a simulated space microgravity environment, and can also simulate a process of landing a planet, learning a course in space teaching, and achieving a planetary landing teaching. purpose.
  • the purpose of the present disclosure is to provide a teaching method, a device, an electronic device and a computer readable storage medium for simulating a planet landing, aiming at solving the operation, teaching and evaluation operations of the spacecraft landing teaching simulating the earth to the planet to be landed.
  • the spacecraft landing orbit information simulating the Earth to the planet to be landed and the spacecraft landing teaching information, dynamically marking the position of the spacecraft on the landing orbit of the simulated Earth to the planet to be landed, after receiving the user spacecraft operation information, Compared with the spacecraft landing orbit information, the spacecraft is prompted to log in the teaching information, and compared with the spacecraft landing operation information, the user's simulation operation state is scored according to the comparison result, and the result of the user's simulation operation state is counted, and then Really simulates the orbit information of the Earth to the planet to be landed, and gives the user a real operational experience, which can deepen the user's learning of the orbits of the various stages of the landing of the planet, and also allows the user to master the spacecraft to simulate the Earth to the landing of the planet.
  • Each technical point has a comprehensive study of the landing process and spacecraft characteristics.
  • the spacecraft landing teaching information corresponding to different track segments is also different.
  • the ascending section orbit it is necessary to monitor the separation of multi-stage rockets and the separation of escape towers. It is necessary to adjust the orbit and attitude of the spacecraft several times when approaching the orbit.
  • landing the orbit it is necessary to know the information of the planet to be landed, the location information of the landing, and the control or detection of other states during the entire landing process of the spacecraft. All of the above can help users to further understand the whole process of landing spacecraft to land on the planet, and enhance the intuitive learning of these spacecraft landing teaching information, which can play a multiplier effect.
  • the present disclosure enhances the user's learning interest by adding points to the user's continuous simulation of the correct behavior.
  • the landing result information is saved as the user's history by using the scoring result and the simulated operation state of the user during the landing process from the simulated earth to the to-be-landed planet. Record the score results of each user logging in to the planet to be registered for the overall data statistics or review by the user in the future.
  • a teaching method for simulating a planet landing including the following steps:
  • Information establishment steps establishing a spacecraft landing orbit information simulating the earth to the planet to be landed and a spacecraft landing teaching information;
  • Position marking step dynamically marking the position of the spacecraft on the landing orbit of the simulated earth to the planet to be landed, and prompting the spacecraft to land the teaching information;
  • Information comparison step receiving the spacecraft landing operation information of the user, comparing the position of the dynamically marked spacecraft on the landing orbit with the spacecraft landing orbit information, and the landing space operation information and the aerospace The device is compared with the teaching information and the comparison results are obtained;
  • State rating step scoring the user's simulated operation state according to the comparison result
  • Result Statistics Step After determining that the spacecraft has landed on the to-be-landed planet, the result of scoring the simulated operation state of the user is counted.
  • the user's simulated operational status is scored according to the comparison result, including:
  • the first scoring sub-step judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the information of the spacecraft landing orbit, and if they are consistent, adding a bonus mark to the simulated operation state of the user; otherwise, the simulation operation on the user Add a minus sign to the status; and,
  • a second scoring sub-step determining whether the spacecraft landing operation information is consistent with the corresponding information in the spacecraft landing teaching information, and if consistent, adding a bonus identifier to the user's simulated operation state; otherwise, the user's simulation operation The status adds a minus sign.
  • the method further includes:
  • a subtraction score for the simulated operation state of the user is calculated based on the deviation value, and the subtraction score is used as the subtraction score.
  • the method further includes: a timeliness detecting step:
  • the method further includes a continuous add-on detecting step:
  • the bonus point identifier After adding a bonus point identifier to the simulated operation state of the user, it is detected whether the bonus point identifier is added to the user's simulated operation state multiple times, and if so, the bonus point value for the user's simulated operation state is increased, and the added value is added.
  • the score is used as an additional bonus marker.
  • the spacecraft landing teaching information includes at least one of rocket separation time information, spacecraft driving information, landing location selection information, and to-go ball information.
  • the spacecraft landing operation information includes at least one of spacecraft direction operation information, power operation information, and spacecraft attitude information.
  • the method further includes: an information saving step:
  • the scoring result and the simulated operation state of the user in the login process from the simulated earth to the to-be-landed planet are used as the history simulation login information of the user and saved.
  • the method further includes a fast forward operation step:
  • the user's historical simulation login information is retrieved;
  • the spacecraft landing orbit information includes rising section orbit information, approaching section orbit information, and landing section orbit information.
  • the method further includes a status display step:
  • the sailing time, sailing mileage, remaining fuel information, remaining mileage, and the remaining navigable time and/or remaining navigable mileage are taken as spacecraft states and displayed.
  • a teaching apparatus for simulating a planetary landing comprising:
  • An information establishing module for establishing a spacecraft landing orbit information simulating the earth to the planet to be landed and a spacecraft landing teaching information
  • a position labeling module configured to dynamically mark the position of the spacecraft on the landing orbit of the simulated earth to the planet to be landed, and prompt the spacecraft to log in the teaching information
  • the information comparison module is configured to receive the spacecraft landing operation information of the user, compare the position of the dynamically marked spacecraft on the landing orbit with the spacecraft landing orbit information, and display the spacecraft operation information and the spacecraft The comparison of the spacecraft landing teaching information and the comparison results;
  • a state scoring module configured to score a simulated operation state of the user according to the comparison result
  • the result statistic module is configured to count the result of scoring the simulated operation state of the user after determining that the spacecraft logs into the to-be-landed planet.
  • an electronic device comprising:
  • a memory having stored thereon computer readable instructions that, when executed by the processor, implement the method of any of the above.
  • a computer readable storage medium having stored thereon a computer program, the computer program being executed by a processor, implements the method of any of the above.
  • the teaching method of simulating a planetary landing in an exemplary embodiment of the present disclosure establishes a spacecraft landing orbit information simulating the earth to the planet to be landed and a spacecraft landing teaching information; dynamically annotating the spacecraft to simulate the earth to the landing orbit of the planet to be landed. a position above, and after receiving the user spacecraft operation information, comparing with the spacecraft landing orbit information, and prompting the spacecraft to log in the teaching information and comparing with the spacecraft landing operation information; The comparison results the user's simulation operation status, and the results of the user's simulation operation status are counted.
  • the real simulation of the orbit information of the Earth to the planet to be landed can deepen the user's learning of the orbits of the various stages of the landing of the planet; on the other hand, through the teaching information on the state of the spacecraft
  • the annotations allow the user to master the technical points of the spacecraft simulating the earth to the landing of the planet to be landed, and have a comprehensive study of the landing process and spacecraft characteristics.
  • FIG. 1 illustrates a flow chart of a teaching method of simulating a planetary landing according to an exemplary embodiment of the present disclosure
  • FIGS. 2A-2B illustrate schematic diagrams of teaching devices simulating a planetary landing, in accordance with an exemplary embodiment of the present disclosure
  • 3A-3D are schematic diagrams showing a state of spacecraft display at various stages of simulated planetary sign-in in a simulated planetary landing teaching device, in accordance with an exemplary embodiment of the present disclosure
  • FIG. 4 shows a schematic block diagram of a teaching device simulating a planetary landing in accordance with an exemplary embodiment of the present disclosure
  • FIG. 5 schematically illustrates a block diagram of an electronic device in accordance with an exemplary embodiment of the present disclosure
  • FIG. 6 schematically illustrates a schematic diagram of a computer readable storage medium in accordance with an exemplary embodiment of the present disclosure.
  • a teaching method for simulating a planet landing is first provided, which can be applied to an electronic device such as a computer; as shown in FIG. 1, the teaching method of the simulated planetary landing may include the following steps:
  • step S110 establishing a spacecraft landing orbit information simulating the earth to the planet to be landed and a spacecraft landing teaching information;
  • Position marking step S120 dynamically marking the position of the spacecraft on the landing orbit of the simulated earth to the planet to be landed, and prompting the spacecraft to log in the teaching information;
  • Information comparison step S130 receiving the spacecraft landing operation information of the user, comparing the position of the dynamically marked spacecraft on the landing orbit with the spacecraft landing orbit information, and the spacecraft landing operation information and the The spacecraft landing teaching information is compared and the results are compared;
  • State scoring step S140 scoring the simulated operation state of the user according to the comparison result
  • Result statistic step S150 After determining that the spacecraft has landed on the to-be-landed planet, the result of scoring the simulated operation state of the user is counted.
  • the teaching method of the simulated planetary landing in the exemplary embodiment since the real simulation of the orbit information of the earth to the landing planet and giving the user a real operational feeling can deepen the user's orbit to the various stages of the landing of the planetary process.
  • the teaching information such as the state of the spacecraft, the user can master the technical points of the spacecraft simulating the earth to the landing of the planet to be landed, and the landing process and spacecraft characteristics are comprehensive. Learning.
  • the spacecraft landing orbit information simulating the earth to the planet to be landed and the spacecraft landing teaching information may be established;
  • the spacecraft landing orbit information simulating the earth to the planet to be landed is first established, and the to-be-landed planet may be a proven planet, such as the moon, Mars, Halley's comet, etc., can also be a virtual data planet for teaching practice.
  • the spacecraft landing orbit information refers to the various components of the spacecraft that are launched from the Earth until the simulating of all orbital information of the planet to be landed.
  • the spacecraft landing orbit information includes rising section orbit information, approaching section orbit information, and landing section orbit information.
  • the spacecraft landing orbit information includes orbital information of the ascending section of the spacecraft from the Earth to the Earth's orbit, and the orbital information of the approaching orbit from the Earth's orbit to the orbiting planet orbit, from the orbiting planet orbit to the landing to the landing Landing track information on the surface of the planet.
  • the orbital segment orbit information may be a combination of multiple orbiting segment orbit information.
  • the spacecraft landing teaching information includes at least one of rocket separation time information, spacecraft driving information, landing location selection information, and to-go ball information. Different instructions and actions are performed in different orbital sections of the spacecraft, and the corresponding spacecraft landing teaching information is also different. For example, in the ascending orbit, the separation of the multi-stage rocket, the separation of the escape tower, etc., and the approaching section are required. In the orbit, it is necessary to adjust the orbit and attitude of the spacecraft multiple times. When landing the orbit, it is necessary to know the information of the planet to be landed, the location information of the landing, and the control or detection of other states during the entire landing process of the spacecraft, such as the remaining amount of fuel, life. Guarantee system status, communication status, antenna angle, etc. All of the above information can help users to further understand the whole process of spacecraft landing on the planet to be landed, and enhance the intuitive learning of these spacecraft landing teaching information, which can achieve a multiplier effect.
  • the position of the spacecraft on the landing orbit of the simulated earth to the planet to be landed may be dynamically marked, and the spacecraft is prompted to land the teaching information;
  • FIG. 2 a schematic display interface of the spacecraft simulating earth to the planetary teaching system to be landed is shown, and the spacecraft including the dynamic annotation display in the figure is on the landing track of the simulated earth to the planet to be landed.
  • Position the position changes dynamically with the user's direction, such as off-track, there will be an alarm prompt, and also includes the spacecraft landing teaching information, which allows the user to quickly understand the current recommended direction operation, etc.
  • Other teaching content information As shown in Fig. 2A, the spacecraft simulates the earth to the schematic display interface of the planetary teaching system to be landed, the spacecraft orbital position information is normal, and there is no direction operation prompt; as shown in Fig. 2B, the spacecraft simulates the earth to the schematic display interface of the planetary teaching system to be landed, The spacecraft is offset from the registration track, and the spacecraft simulates the display interface of the earth to the landing teaching system to display the prompt direction operation information.
  • the spacecraft landing operation information of the user may be received, the position of the dynamically marked spacecraft on the landing orbit is compared with the spacecraft landing orbit information, and the spacecraft landing operation information is Compare with the spacecraft landing teaching information and obtain comparison results;
  • the spacecraft landing operation information of the user after receiving the spacecraft landing operation information of the user, mainly the direction operation information of the user, generating the corresponding displacement of the direction operation information on the landing track of the spacecraft, and then dynamically marking the The position of the spacecraft on the landing orbit is compared with the information of the spacecraft landing orbit, and the difference between the theoretical position and the actual position is compared.
  • the state or control operation is compared with the spacecraft landing teaching information.
  • the spacecraft landing operation information includes at least one of spacecraft direction operation information, power operation information, and spacecraft attitude information.
  • the spacecraft landing operation information includes the spacecraft direction operation information for controlling the spacecraft direction, the power operation information for controlling the spacecraft speed, and the spacecraft attitude information for controlling the space attitude. Further, it also includes rocket separation information, spacecraft docking information, and the like.
  • the simulated operation state of the user may be scored according to the comparison result
  • the state scoring step S140 may include a first scoring sub-step S1401 and a second scoring sub-step S1402.
  • the first scoring sub-step S1401 judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the spacecraft landing orbit information, and if they are consistent, adding a bonus point to the user's simulated operation state; otherwise, simulating the user Add a subtraction identifier to the operational status; and,
  • a second scoring sub-step S1402 determining whether the spacecraft landing operation information is consistent with the corresponding information in the spacecraft landing teaching information, and if they are consistent, adding a bonus identifier to the user's simulated operation state; otherwise, simulating the user Add a subtraction ID to the operational status.
  • the scoring of the simulated operation state of the user according to the comparison result is one of the methods for evaluating the teaching achievement, and the user's learning mastery degree can be quickly understood, and the user's learning interest can also be improved. Different scores can be set according to the difficulty level of the spacecraft landing teaching information.
  • the bonus mark or the subtraction mark can be zero-pointed, that is, all users can be uniformly added without deducting points or only deducting points without adding points.
  • the method further includes a continuous add-on detection step: after adding a bonus identifier to the simulated operation state of the user, detecting whether the add-on identifier is added to the simulated operation state of the user multiple times, and if so, increasing A score is added to the user's simulated operational state, and the added bonus score is used as an additional bonus identifier.
  • a continuous add-on detection step after adding a bonus identifier to the simulated operation state of the user, detecting whether the add-on identifier is added to the simulated operation state of the user multiple times, and if so, increasing A score is added to the user's simulated operational state, and the added bonus score is used as an additional bonus identifier.
  • the method further includes: determining the position of the dynamically marked spacecraft on the landing orbit. Inconsistent with the spacecraft landing orbit information, detecting a deviation value between the two; calculating a subtraction score for the simulated operation state of the user according to the deviation value, and using the subtraction score as the reduction score Logo.
  • different scores may be set according to the difficulty level of the spacecraft landing teaching information.
  • the implementation degree of different spacecraft landing operation information corresponding to the same spacecraft landing teaching information may be different, and the level difference may also be set. Reflecting the accuracy of the spacecraft landing operation information. Specifically, the deviation value between the position of the spacecraft on the landing orbit and the information of the spacecraft landing orbit can be detected, and the accuracy of the operation information of the spacecraft landing direction is measured by the deviation value.
  • the method further includes: if determining the spacecraft landing operation information and the aerospace Corresponding information in the landing teaching information is consistent, detecting the user's timeliness of the spacecraft landing operation; calculating a bonus score for the user's simulated operating state according to the timeliness, and using the added score as the Extra points.
  • the timeliness of the user's landing operation can be detected, and the accuracy of the spacecraft landing operation information is measured by the timeliness.
  • the method further includes detecting the order and coordination degree of the user's landing operations on the plurality of spacecrafts, and also measuring the accuracy of the spacecraft landing operation information.
  • the result statistics step S150 after the spacecraft is determined to log in to the to-be-landed planet, the result of scoring the simulated operation state of the user may be counted.
  • the total score is calculated according to the scores of the spacecraft landing operation information described above, and the level of the user's simulation of the earth to the planet to be landed is measured. Meanwhile, if the user finishes logging in to the to-be-landed planet for the first time, the to-be-landed planet is marked as the user's landed planet.
  • it may also include a score that fails to successfully log in to the to-be-landed planet due to an erroneous operation. And after successfully landing to the to-be-landed planet, simulating the score of the operation of returning to the earth from the planet to be landed.
  • the method further includes: using the scoring result and the simulated operation state of the user in the login process from the simulated earth to the to-be-landed planet as the history of the user. Simulate login information and save it. Record the score results of each user logging in to the planet to be registered each time for overall data statistics or review by the user in the future.
  • the method further includes: when detecting that the current spacecraft landing mode is the repeated learning mode, retrieving the historical simulation login information of the user; performing the current login operation phase of the user and the historical simulation login information. Matching, when determining that the current login operation phase is the correct operation phase in the historical simulation login information, sending an inquiry instruction to the user whether to fast forward; after receiving the confirmation fast forward instruction of the user reply, the flow of the correct operation phase is performed.
  • Fast forward operation The teaching method of simulating the earth to the landing of the planet to be landed may have a review function, so that the user can quickly retrieve the historical simulation login information, and the information may be specially marked with historical error operation information, and the historical error operation information is emphasized. The operation is reviewed, and there may be a fast forward command for other operational information to fast forward the flow of the correct operational phase that does not require review.
  • the method further includes: calculating remaining fuel information of the spacecraft according to the time of the spacecraft, the sailing mileage, and the preset spacecraft fuel information; acquiring the remaining mileage of the earth to the planet to be landed; The remaining fuel information and the remaining mileage calculate the remaining navigable time and/or remaining navigable mileage; the sailing time, sailing mileage, remaining fuel information, remaining mileage, and the remaining navigable time and/or The remaining navigable mileage is displayed as a spacecraft state.
  • the spacecraft state display interface may be a static display of the spacecraft's navigation time, sailing mileage, and spacecraft fuel information, and may display a warning flag when the remaining fuel is insufficient to complete the next mission.
  • the simulated lunar registration teaching device is in the take-off stage, the first stage rocket is in the ignition countdown state, and the other devices are in normal state, no alarm information is displayed; as shown in Fig. 3B, the simulated lunar registration teaching device is in the near flight stage, and the display is shown.
  • the first stage rocket and the second stage rocket have been separated.
  • the first stage rocket has completed the recovery function, the service compartment is in the alarm state, the alarm information is low voltage, and the other devices are in normal state; as shown in Fig.
  • the simulated moon login teaching device is registered on the moon.
  • the landing cabin has been separated from the command cabin and the service cabin.
  • the state is in the lunar log, the command and service cabins are on standby in the lunar orbit, and the service compartment is in the alarm state; as shown in Figure 3D, the simulated lunar registration teaching device returns.
  • the command module returns to the earth, and the remaining devices are separated except for the first stage rocket has been recovered, the returning state is normal, and no alarm information is displayed.
  • the simulated planetary landing teaching device 400 can include an information establishing module 410, a location labeling module 420, an information comparison module 430, a status scoring module 440, and a result statistics module 450. among them:
  • the information establishing module 410 is configured to establish a spacecraft landing orbit information simulating the earth to the planet to be landed and a spacecraft landing teaching information;
  • the location labeling module 420 is configured to dynamically mark the position of the spacecraft on the landing orbit of the simulated earth to the planet to be landed, and prompt the spacecraft to log in the teaching information;
  • the information comparison module 430 is configured to receive the spacecraft landing operation information of the user, compare the position of the dynamically marked spacecraft on the landing orbit with the spacecraft landing orbit information, and compare the spacecraft landing operation information with the spacecraft The spacecraft landing teaching information is compared and the comparison results are obtained;
  • a state scoring module 440 configured to score a simulated operation state of the user according to the comparison result
  • the result statistic module 450 is configured to count the result of scoring the simulated operation state of the user after determining that the spacecraft logs into the to-be-landed planet.
  • modules or units of the teaching device 400 simulating a planetary landing are mentioned in the detailed description above, such division is not mandatory. Indeed, in accordance with embodiments of the present disclosure, the features and functions of two or more modules or units described above may be embodied in one module or unit. Conversely, the features and functions of one of the modules or units described above may be further divided into multiple modules or units.
  • an electronic device capable of implementing the above method is also provided.
  • aspects of the present invention can be implemented as a system, method, or program product. Accordingly, aspects of the present invention may be embodied in the form of a complete hardware embodiment, a complete software embodiment (including firmware, microcode, etc.), or a combination of hardware and software aspects, which may be collectively referred to herein. "Circuit,” “module,” or “system.”
  • FIG. 5 An electronic device 500 in accordance with such an embodiment of the present invention is described below with reference to FIG. 5 is merely an example and should not impose any limitation on the function and scope of use of the embodiments of the present invention.
  • electronic device 500 is embodied in the form of a general purpose computing device.
  • the components of the electronic device 500 may include, but are not limited to, the at least one processing unit 510, the at least one storage unit 520, the bus 530 connecting the different system components (including the storage unit 520 and the processing unit 510), and the display unit 540.
  • the storage unit stores program code, which can be executed by the processing unit 510, such that the processing unit 510 performs various exemplary embodiments according to the present invention described in the "Exemplary Method" section of the present specification.
  • the processing unit 510 can perform steps S110 to S150 as shown in FIG. 1.
  • the storage unit 520 can include a readable medium in the form of a volatile storage unit, such as a random access storage unit (RAM) 5201 and/or a cache storage unit 5202, and can further include a read only storage unit (ROM) 5203.
  • RAM random access storage unit
  • ROM read only storage unit
  • the storage unit 520 can also include a program/utility 5204 having a set (at least one) of the program modules 5205, such as but not limited to: an operating system, one or more applications, other program modules, and program data, Implementations of the network environment may be included in each or some of these examples.
  • a program/utility 5204 having a set (at least one) of the program modules 5205, such as but not limited to: an operating system, one or more applications, other program modules, and program data, Implementations of the network environment may be included in each or some of these examples.
  • Bus 530 may be representative of one or more of several types of bus structures, including a memory unit bus or memory unit controller, a peripheral bus, a graphics acceleration port, a processing unit, or a local area using any of a variety of bus structures. bus.
  • the electronic device 500 can also communicate with one or more external devices 570 (eg, a keyboard, pointing device, Bluetooth device, etc.), and can also communicate with one or more devices that enable the user to interact with the electronic device 500, and/or with Any device (eg, router, modem, etc.) that enables the electronic device 500 to communicate with one or more other computing devices. This communication can take place via an input/output (I/O) interface 550. Also, electronic device 500 can communicate with one or more networks (e.g., a local area network (LAN), a wide area network (WAN), and/or a public network, such as the Internet) via network adapter 560. As shown, network adapter 560 communicates with other modules of electronic device 500 via bus 530.
  • network adapter 560 communicates with other modules of electronic device 500 via bus 530.
  • the exemplary embodiments described herein may be implemented by software, or may be implemented by software in combination with necessary hardware. Therefore, the technical solution according to an embodiment of the present disclosure may be embodied in the form of a software product, which may be stored in a non-volatile storage medium (which may be a CD-ROM, a USB flash drive, a mobile hard disk, etc.) or on a network.
  • a non-volatile storage medium which may be a CD-ROM, a USB flash drive, a mobile hard disk, etc.
  • a number of instructions are included to cause a computing device (which may be a personal computer, server, terminal device, or network device, etc.) to perform a method in accordance with an embodiment of the present disclosure.
  • a computer readable storage medium having stored thereon a program product capable of implementing the above method of the present specification.
  • aspects of the present invention may also be embodied in the form of a program product comprising program code for causing said program product to run on a terminal device
  • the terminal device performs the steps according to various exemplary embodiments of the present invention described in the "Exemplary Method" section of the present specification.
  • a program product 600 for implementing the above method which may employ a portable compact disk read only memory (CD-ROM) and includes program code, and may be in a terminal device, is illustrated in accordance with an embodiment of the present invention.
  • the program product of the present invention is not limited thereto, and in the present document, the readable storage medium may be any tangible medium containing or storing a program that can be used by or in connection with an instruction execution system, apparatus or device.
  • the program product can employ any combination of one or more readable media.
  • the readable medium can be a readable signal medium or a readable storage medium.
  • the readable storage medium can be, for example, but not limited to, an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any combination of the above. More specific examples (non-exhaustive lists) of readable storage media include: electrical connections with one or more wires, portable disks, hard disks, random access memory (RAM), read only memory (ROM), erasable Programmable read-only memory (EPROM or flash memory), optical fiber, portable compact disk read only memory (CD-ROM), optical storage device, magnetic storage device, or any suitable combination of the foregoing.
  • the computer readable signal medium may include a data signal that is propagated in the baseband or as part of a carrier, carrying readable program code. Such propagated data signals can take a variety of forms including, but not limited to, electromagnetic signals, optical signals, or any suitable combination of the foregoing.
  • the readable signal medium can also be any readable medium other than a readable storage medium that can transmit, propagate, or transport a program for use by or in connection with an instruction execution system, apparatus, or device.
  • Program code embodied on a readable medium can be transmitted using any suitable medium, including but not limited to wireless, wireline, optical cable, RF, etc., or any suitable combination of the foregoing.
  • Program code for performing the operations of the present invention may be written in any combination of one or more programming languages, including an object oriented programming language such as Java, C++, etc., including conventional procedural Programming language—such as the "C" language or a similar programming language.
  • the program code can execute entirely on the user computing device, partially on the user device, as a stand-alone software package, partially on the remote computing device on the user computing device, or entirely on the remote computing device or server. Execute on.
  • the remote computing device can be connected to the user computing device via any kind of network, including a local area network (LAN) or wide area network (WAN), or can be connected to an external computing device (eg, provided using an Internet service) Businesses are connected via the Internet).
  • LAN local area network
  • WAN wide area network
  • Businesses are connected via the Internet.
  • the real simulation of the orbit information of the Earth to the planet to be landed can deepen the user's learning of the orbits of the various stages of the landing of the planet; on the other hand, through the teaching information on the state of the spacecraft
  • the annotations allow the user to master the technical points of the spacecraft simulating the earth to the landing of the planet to be landed, and have a comprehensive study of the landing process and spacecraft characteristics.

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Abstract

本公开是关于一种模拟星球登陆的教学方法、装置、电子设备以及存储介质。其中，该方法包括：建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并在接收到用户航天器操作信息后，与所述航天器登陆轨道信息对比，以及，提示所述航天器登陆教学信息，并与所述航天器登陆操作信息对比；根据所述对比结果对用户的模拟操作状态进行评分，并统计对用户的模拟操作状态的评分结果。本公开可以实现地球至待登陆星球的航天器模拟星球登陆的教学。

Description

模拟星球登陆的教学方法以及装置 技术领域
本公开涉及计算机技术领域，具体而言，涉及一种模拟星球登陆的教学方法、装置、电子设备以及计算机可读存储介质。
背景技术
目前，随着人类科技的高速进步发展，对宇宙未知空间的探索也越来越被更多的人关注，特别是从地球出发，登陆到其它星球，成了许多的梦想，所以对如何进行星球登陆的教学的问题也随之而来。高质量的星球登陆的教学，可以激发人们对外太空探索的兴趣，也可以增强人们对宇宙其他星球的了解。
然而，现有对模拟星球登陆的方法都还仅是初步的探索阶段，一般以模拟太空微重力环境以及游戏体验为主，并不能达到教学的目的。例如：
申请号为CN201710159287.6的专利申请公开了一种青少年国防航天教育专用的模拟太空舱系统，以及公开了该系统中的基础设施，包括太空舱、舱壁护垫、内舱地板、逃遁舱、左侧推进器、右侧推进器、进舱门、进舱开关旋转把手等等，其目的在于：利用模拟太空舱系统展现航天文化和航天科技生成逼真的太空模拟环境，让青少年可以通过模拟的太空设施和太空舱环境体验太空无重状态和倒转回旋的太空生活体验。该申请仅仅公开了一种青少年航天教育专用的模拟太空舱系统的硬件设施，其仅能为青少年提供对于太空环境的微重力感官体验，并不能达到为用户提供星球登陆过程中的教学目的。
申请号为CN201210484568.6的专利申请公开了一种空间微重力模拟实验系统，主要包括外围框架、调平系统、水平面内被动调节机构、Z方向主动重力补偿系统、回转被动调整机构以及俯仰偏转主动调整系统，并通过各部件之间的配合模拟太空微重力环境，完成实验对象姿态的变化，复现零重力状态。
申请号为CN03276220.8的专利申请公开了一种模拟航天器，通过电脑集中控制，根据航天的进程，电视机播放的“窗外”情景、声响，同本实用新型的碰撞、震动，以及飞行仓2的飞行角度、仓内温度吻合一致，使游客逼真地感受到太空飞行的体验，感受倾斜、拐弯、碰撞、摇晃、旋转等多种航天动作。
申请号为CN92200996.1的“一种娱乐太空船”，利用万向连接轴与升降器等，使人在运动感觉、环境感觉和观察感觉上满足邀游太空的模拟需要。
申请号为CN00234436.X的“磁悬浮太空娱乐船”，利用船底的高强磁铁和运行滑道上的高强磁铁使娱乐船处于悬浮状态，娱乐船中的游客沿高坡自然顺坡下滑时，产生太空邀游的感觉。
在上述现有技术中，都只是单纯的对航天器的模拟，模拟太空微重力环境或者使用户进行太空游戏体验，关于模拟星球登陆中的教学还存在以下问题：
不能为用户提供航天器模拟地球登陆待登陆星球过程中的技术要点、测评，更不能完成模拟宇航员星球登陆过程中的学习，无法达到星球登陆教学的目的。
本公开针对现有技术中存在的上述问题，主要为了使用户在模拟太空微重力环境下进行太空体验的基础上，还可以模拟星球登陆的过程，学习太空教学方面的课程，达到星球登陆教学的目的。
需要说明的是，在上述背景技术部分公开的信息仅用于加强对本公开的背景的理解，因此可以包括不构成对本领域普通技术人员已知的现有技术的信息。
发明内容
本公开的目的在于提供一种模拟星球登陆的教学方法、装置、电子设备以及计算机可读存储介质，旨在解决模拟地球至待登陆星球的航天器登 陆教学中的体验、教学以及测评等操作学习，让用户掌握航天器模拟地球至待登陆星球登陆整个过程中各个技术要点，特别是对登陆过程、航天器特性都有比较全面的学习。本发明的改进包括以下内容：
通过预先建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息，动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，在接收到用户航天器操作信息后，与航天器登陆轨道信息对比、提示航天器登陆教学信息，并与航天器登陆操作信息对比，根据对比结果对用户的模拟操作状态进行评分，并统计对用户的模拟操作状态的评分结果，进而可以真实的模拟了地球至待登陆星球的轨道信息，并给予用户真实的操作感受，可以加深用户对登陆星球过程各阶段轨道的学习，还可以让用户掌握航天器模拟地球至待登陆星球登陆整个过程中各个技术要点，对登陆过程、航天器特性都有比较全面的学习。
通过在航天器不同轨道段设置不同执行指令和动作，使不同轨道段对应的航天器登陆教学信息也不同，如在上升段轨道时，需要对多级火箭的分离，逃逸塔的分离等监控，迫近段轨道时需要多次对航天器轨道、姿态进行调整，登陆段轨道时需要了解待登陆星球信息、登陆位置信息，以及在航天器整个登陆过程中其它状态的控制或检测等。以上均可以帮助用户更加深入的学习体会航天器登陆待登陆星球的整个过程，加强对这些航天器登陆教学信息的直观学习，可以起到事半功倍的教学效果。
在判断航天器登陆操作信息与航天器登陆教学信息中的对应信息是否一致后，在确定航天器登陆操作信息与航天器登陆教学信息中的对应信息一致时，检测用户对航天器登陆操作的及时度，根据及时度计算对用户的模拟操作状态的加分分值，进而衡量航天器登陆操作信息的准确程度。
通过对用户的模拟操作状态添加加分标识，并在检测对用户的模拟操作状态连续多次添加加分标识后，还可以增加对用户的模拟操作状态的加分分值，并将增加的加分分值作为额外的加分标识。本公开为增强教学体验，通过对用户连续模拟操作正确的行为进行加分奖励，进而提升用户的学习兴趣。
在统计对用户的模拟操作状态的评分结果后，通过将评分结果以及从模拟地球至待登陆星球的登陆过程中用户的模拟操作状态作为用户的历史模拟登陆信息并保存。记录每个用户每次登陆待登陆星球的评分结果，以供整体数据统计或用户日后复习查阅。
根据本公开的一个方面，提供一种模拟星球登陆的教学方法，包括以下步骤：
信息建立步骤：建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；
位置标注步骤：动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并提示所述航天器登陆教学信息；
信息对比步骤：接收用户的航天器登陆操作信息，将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，以及，将所述航天器登陆操作信息与所述航天器登陆教学信息对比，并得到对比结果；
状态评分步骤：根据所述对比结果对用户的模拟操作状态进行评分；
结果统计步骤：在确定所述航天器登陆所述待登陆星球后，统计对用户的模拟操作状态的评分结果。
在本公开的一种示例性实施例中，根据所述对比结果对用户的模拟操作状态进行评分，包括：
第一评分子步骤：判断动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息是否一致，若一致，对用户的模拟操作状态添加加分标识，否则，对用户的模拟操作状态添加减分标识；以及，
第二评分子步骤：判断所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息是否一致，若一致，对用户的模拟操作状态添加加分标识，否则，对用户的模拟操作状态添加减分标识。
在本公开的一种示例性实施例中，在判断动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息是否一致后，所述方法还包括：
若确定动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道 信息不一致，检测两者之间的偏差值；
根据所述偏差值计算对用户的模拟操作状态的减分分值，并将所述减分分值作为所述减分标识。
在本公开的一种示例性实施例中，在判断所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息是否一致后，所述方法还包括，及时度检测步骤：
若确定所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息一致，检测用户对航天器登陆操作的及时度；
根据所述及时度计算对用户的模拟操作状态的加分分值，并将所述加分分值作为所述加分标识。
在本公开的一种示例性实施例中，所述方法还包括，连续加分检测步骤：
在对用户的模拟操作状态添加加分标识后，检测是否对用户的模拟操作状态连续多次添加加分标识，若是，则增加对用户的模拟操作状态的加分分值，并将增加的加分分值作为额外的加分标识。
在本公开的一种示例性实施例中，所述航天器登陆教学信息包括火箭分离时间信息、航天器驾驶信息、登陆位置选择信息、待登陆星球信息的至少一项。
在本公开的一种示例性实施例中，所述航天器登陆操作信息包括航天器方向操作信息、动力操作信息，航天器姿态信息的至少一项。
在本公开的一种示例性实施例中，统计对用户的模拟操作状态的评分结果后，所述方法还包括，信息保存步骤：
将所述评分结果以及从模拟地球至待登陆星球的登陆过程中用户的模拟操作状态作为用户的历史模拟登陆信息并保存。
在本公开的一种示例性实施例中，所述方法还包括，快进操作步骤：
在检测到当前的航天器登陆模式为重复学习模式时，调取用户的历史模拟登陆信息；
将用户当前登陆操作阶段与所述历史模拟登陆信息进行匹配，在确定当前登陆操作阶段为历史模拟登陆信息中的正确操作阶段时，向用户发送是否快进的询问指令；
在接收到用户回复的确认快进指令后，将所述正确操作阶段的流程进行快进操作。
在本公开的一种示例性实施例中，所述航天器登陆轨道信息包括上升段轨道信息、迫近段轨道信息和登陆段轨道信息。
在本公开的一种示例性实施例中，所述方法还包括，状态显示步骤：
根据航天器的航行时间、航行里程以及预设的航天器燃料信息计算所述航天器的剩余燃料信息；
获取地球至待登陆星球的剩余里程；
根据所述剩余燃料信息以及所述剩余里程计算所述剩余可航行时间和/或剩余可航行里程；
将所述航行时间、航行里程、剩余燃料信息、剩余里程以及所述剩余可航行时间和/或剩余可航行里程作为航天器状态，并显示。
在本公开的一个方面，提供一种模拟星球登陆的教学装置，包括：
信息建立模块，用于建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；
位置标注模块，用于动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并提示所述航天器登陆教学信息；
信息对比模块，用于接收用户的航天器登陆操作信息，将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，以及，将所述航天器登陆操作信息与所述航天器登陆教学信息对比，并得到对比结果；
状态评分模块，用于根据所述对比结果对用户的模拟操作状态进行评分；
结果统计模块，用于在确定所述航天器登陆所述待登陆星球后，统计 对用户的模拟操作状态的评分结果。
在本公开的一个方面，提供一种电子设备，包括：
处理器；以及
存储器，所述存储器上存储有计算机可读指令，所述计算机可读指令被所述处理器执行时实现根据上述任意一项所述的方法。
在本公开的一个方面，提供一种计算机可读存储介质，其上存储有计算机程序，所述计算机程序被处理器执行时实现根据上述任意一项所述的方法。
本公开的示例性实施例中的模拟星球登陆的教学方法，建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并在接收到用户航天器操作信息后，与所述航天器登陆轨道信息对比，以及，提示所述航天器登陆教学信息，并与所述航天器登陆操作信息对比；根据所述对比结果对用户的模拟操作状态进行评分，并统计对用户的模拟操作状态的评分结果。一方面，由于真实的模拟了地球至待登陆星球的轨道信息，并给予用户真实的操作感受，可以加深用户对登陆星球过程各阶段轨道的学习；另一方面，通过对航天器状态等教学信息的标注，可以让用户掌握航天器模拟地球至待登陆星球登陆整个过程中各个技术要点，对所述登陆过程、航天器特性都有比较全面的学习。
应当理解的是，以上的一般描述和后文的细节描述仅是示例性和解释性的，并不能限制本公开。
附图说明
通过参照附图来详细描述其示例实施例，本公开的上述和其它特征及优点将变得更加明显。
图1示出了根据本公开一示例性实施例的模拟星球登陆的教学方法的流程图；
图2A-2B示出了根据本公开一示例性实施例的模拟星球登陆的教学装置的示意图；
图3A-3D示出了根据本公开一示例性实施例的模拟星球登陆的教学装置在模拟星球登录各阶段显示航天器状态的示意图；
图4示出了根据本公开一示例性实施例的模拟星球登陆的教学装置的示意框图；
图5示意性示出了根据本公开一示例性实施例的电子设备的框图；以及
图6示意性示出了根据本公开一示例性实施例的计算机可读存储介质的示意图。
具体实施方式
现在将参考附图更全面地描述示例实施例。然而，示例实施例能够以多种形式实施，且不应被理解为限于在此阐述的实施例；相反，提供这些实施例使得本公开将全面和完整，并将示例实施例的构思全面地传达给本领域的技术人员。在图中相同的附图标记表示相同或类似的部分，因而将省略对它们的重复描述。
此外，所描述的特征、结构或特性可以以任何合适的方式结合在一个或更多实施例中。在下面的描述中，提供许多具体细节从而给出对本公开的实施例的充分理解。然而，本领域技术人员将意识到，可以实践本公开的技术方案而没有所述特定细节中的一个或更多，或者可以采用其它的方法、组元、材料、装置、步骤等。在其它情况下，不详细示出或描述公知结构、方法、装置、实现、材料或者操作以避免模糊本公开的各方面。
附图中所示的方框图仅仅是功能实体，不一定必须与物理上独立的实体相对应。即，可以采用软件形式来实现这些功能实体，或在一个或多个软件硬化的模块中实现这些功能实体或功能实体的一部分，或在不同网络和/或处理器装置和/或微控制器装置中实现这些功能实体。
在本示例实施例中，首先提供了一种模拟星球登陆的教学方法，可以应用于计算机等电子设备；参考图1中所示，该模拟星球登陆的教学方法可以包括以下步骤：
信息建立步骤S110：建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；
位置标注步骤S120：动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并提示所述航天器登陆教学信息；
信息对比步骤S130：接收用户的航天器登陆操作信息，将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，以及，将所述航天器登陆操作信息与所述航天器登陆教学信息对比，并得到对比结果；
状态评分步骤S140：根据所述对比结果对用户的模拟操作状态进行评分；
结果统计步骤S150：在确定所述航天器登陆所述待登陆星球后，统计对用户的模拟操作状态的评分结果。
根据本示例实施例中的模拟星球登陆的教学方法，一方面，由于真实的模拟了地球至待登陆星球的轨道信息，并给予用户真实的操作感受，可以加深用户对登陆星球过程各阶段轨道的学习；另一方面，通过对航天器状态等教学信息的标注，可以让用户掌握航天器模拟地球至待登陆星球登陆整个过程中各个技术要点，对所述登陆过程、航天器特性都有比较全面的学习。
下面，将对本示例实施例中的模拟星球登陆的教学方法进行进一步的说明。
在信息建立步骤S110中，可以建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；
本示例实施方式中，要进行航天器模拟登陆星球的教学就先要建立模拟地球至待登陆星球的航天器登陆轨道信息，所述待登陆星球可以是已经 探明的行星，如月球、火星、哈雷彗星等，也可以是为了教学实践，建立的虚拟数据的星球。所述航天器登陆轨道信息是指航天器的各个部件从地球发射，直至成功模拟登陆待登陆星球的全部轨道信息。
在航天器模拟地球至待登陆星球的登陆过程，会执行不同的指令，完成不同的动作，来实现航天器的成功登陆，而所述指令和动作都可以是航天器登陆教学信息，可以让用户学习体会到航天器模拟登陆的整个过程。
本示例实施方式中，所述航天器登陆轨道信息包括上升段轨道信息、迫近段轨道信息和登陆段轨道信息。航天器登陆轨道信息包括航天器从地球发射至地球轨道的上升段轨道信息，从地球轨道至所述待登陆星球轨道的迫近段轨道信息，从所述待登陆星球轨道至登陆到所述待登陆星球表面的登陆段轨道信息。当登陆距离较远、或迫近方式复杂如需多次环绕第三星球、或利用引力弹弓的待登陆星球时，所述迫近段轨道信息可以是多个迫近段轨道信息的组合。
本示例实施方式中，所述航天器登陆教学信息包括火箭分离时间信息、航天器驾驶信息、登陆位置选择信息、待登陆星球信息的至少一项。在航天器不同轨道段所执行的指令和动作不同，对应的所述航天器登陆教学信息也不同，如在上升段轨道时，需要对多级火箭的分离，逃逸塔的分离等监控，迫近段轨道时需要多次对航天器轨道、姿态进行调整，登陆段轨道时需要了解待登陆星球信息、登陆位置信息，以及在航天器整个登陆过程中其它状态的控制或检测，如燃料剩余量、生命保障系统状态、通讯状态、天线角度等。上述这些信息都可以帮助用户更加深入的学习体会航天器登陆待登陆星球的整个过程，加强对这些航天器登陆教学信息的直观学习，可以起到事半功倍的教学效果。
在位置标注步骤S120中，可以动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并提示所述航天器登陆教学信息；
本示例实施方式中，如图2所示为航天器模拟地球至待登陆星球教学系统的示意显示界面，在图中包含动态标注显示的航天器在所述模拟地球至待登陆星球的登陆轨道上的位置，所述位置随用户的方向操作而动态变 化，如脱离轨道，会有报警提示，还包含了所述航天器登陆教学信息，可以让用户快捷的了解到当前推荐的方向操作等，以及其它教学内容信息。如图2A航天器模拟地球至待登陆星球教学系统的示意显示界面中，航天器轨道位置信息正常，无方向操作提示；如图2B航天器模拟地球至待登陆星球教学系统的示意显示界面中，航天器偏移出所述登录轨道，所述航天器模拟地球至待登陆星球教学系统中的显示界面显示提示方向操作信息。
在信息对比步骤S130中，可以接收用户的航天器登陆操作信息，将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，以及，将所述航天器登陆操作信息与所述航天器登陆教学信息对比，并得到对比结果；
本示例实施方式中，在接收到用户的航天器登陆操作信息，主要是用户的方向操作信息后，将所述方向操作信息生成相应的位移在航天器的登陆轨道上显示，然后将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，比较理论位置与实际位置的差值。同时，在接收到在接收到用户的航天器登陆操作信息，主要是状态或控制操作信息后，将所述状态或控制操作与所述航天器登陆教学信息对比。
本示例实施方式中，所述航天器登陆操作信息包括航天器方向操作信息、动力操作信息，航天器姿态信息的至少一项。航天器登陆操作信息包括控制航天器方向的航天器方向操作信息、控制航天器速度的动力操作信息，控制航天姿态的航天器姿态信息等。进一步的，还包括火箭分离信息、航天器对接信息等。
在状态评分步骤S140中，可以根据所述对比结果对用户的模拟操作状态进行评分；
其中，状态评分步骤S140可以包括第一评分子步骤S1401以及第二评分子步骤S1402。
第一评分子步骤S1401：判断动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息是否一致，若一致，对用户的模拟操作状态添加加分标识，否则，对用户的模拟操作状态添加减分标识；以及，
第二评分子步骤S1402：判断所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息是否一致，若一致，对用户的模拟操作状态添加加分标识，否则，对用户的模拟操作状态添加减分标识。
本示例实施方式中，根据所述对比结果对用户的模拟操作状态进行评分是对教学成果评价的方法之一，可以快捷的了解用户的学习掌握程度，也可以提升用户的学习兴趣。根据航天器登陆教学信息的难易程度可以设置不同的分值。同时，所述加分标识或减分标识都可以零分，也就是可以所有用户统一只加分不扣分或只扣分不加分。
本示例实施方式中，所述方法还包括连续加分检测步骤：在对用户的模拟操作状态添加加分标识后，检测是否对用户的模拟操作状态连续多次添加加分标识，若是，则增加对用户的模拟操作状态的加分分值，并将增加的加分分值作为额外的加分标识。为增强教学体验，可以对用户连续模拟操作正确的行为进行加分奖励，提升用户的学习兴趣。
本示例实施方式中，在判断动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息是否一致后，所述方法还包括：若确定动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息不一致，检测两者之间的偏差值；根据所述偏差值计算对用户的模拟操作状态的减分分值，并将所述减分分值作为所述减分标识。前述了根据航天器登陆教学信息的难易程度可以设置不同的分值，同时，针对同一航天器登陆教学信息对应的不同的航天器登陆操作信息的实现程度不同，也可以设置等级的分差，体现所述航天器登陆操作信息的准确程度。具体的，可以检测航天器在登陆轨道上的位置与所述航天器登陆轨道信息之间的偏差值，以所述偏差值来衡量所述航天器登陆方向操作信息的准确程度。
本示例实施方式中，在判断所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息是否一致后，所述方法还包括：若确定所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息一致，检测用户对航天器登陆操作的及时度；根据所述及时度计算对用户的模拟操作状态的加分分值，并将所述加分分值作为所述加分标识。可以检测用户对航天器登陆操作的及时度，以所述及时度来衡量所述航天器登陆操作信息的准 确程度。进一步的，还包括检测用户对多个航天器登陆操作的顺序、协调程度，并也以此来衡量所述航天器登陆操作信息的准确程度。
在结果统计步骤S150中，可以在确定所述航天器登陆所述待登陆星球后，统计对用户的模拟操作状态的评分结果。
本示例实施方式中，根据上述各航天器登陆操作信息的评分计算总分，并以此来衡量所述用户此次模拟地球至待登陆星球过程的水平。同时，若所述用户是第一次完成对所述待登陆星球的登陆，则将所述待登陆星球标记为所述用户的已登陆星球。
本示例实施方式中，还可以包括对因错误操作而未能成功登陆至所述待登陆星球的评分。以及成功登陆至所述待登陆星球后，模拟从所述待登陆星球返回地球过程的操作的评分。
本示例实施方式中，统计对用户的模拟操作状态的评分结果后，所述方法还包括：将所述评分结果以及从模拟地球至待登陆星球的登陆过程中用户的模拟操作状态作为用户的历史模拟登陆信息并保存。记录每个用户每次登陆所述待登陆星球的评分结果，以供整体数据统计或用户日后复习查阅。
本示例实施方式中，所述方法还包括：在检测到当前的航天器登陆模式为重复学习模式时，调取用户的历史模拟登陆信息；将用户当前登陆操作阶段与所述历史模拟登陆信息进行匹配，在确定当前登陆操作阶段为历史模拟登陆信息中的正确操作阶段时，向用户发送是否快进的询问指令；在接收到用户回复的确认快进指令后，将所述正确操作阶段的流程进行快进操作。所述模拟地球至待登陆星球登陆的教学方法可以有复习功能，使用户快捷的调取历史模拟登陆信息，所述信息中可以特殊标记出历史错误操作信息，着重对所述历史错误操作信息进行复习操作，而对其它操作信息可以有快进指令，以将所述不需要复习的正确操作阶段的流程进行快进操作。
本示例实施方式中，所述方法还包括：根据航天器的航行时间、航行里程以及预设的航天器燃料信息计算所述航天器的剩余燃料信息；获取地 球至待登陆星球的剩余里程；根据所述剩余燃料信息以及所述剩余里程计算所述剩余可航行时间和/或剩余可航行里程；将所述航行时间、航行里程、剩余燃料信息、剩余里程以及所述剩余可航行时间和/或剩余可航行里程作为航天器状态，并显示。所述航天器状态显示界面可以是静态显示航天器的航行时间、航行里程以及航天器燃料信息，并可以在剩余燃料不足以完成下次任务时，显示警告标记。为增强用户的航天器模拟地球至所述待登陆星球的登陆过程的教学体验，也可以是三维动画的方式显示。如图3A所示为模拟月球登录教学装置待起飞阶段，一级火箭为点火倒计时状态，其余装置状态正常，无报警信息显示；如图3B所示为模拟月球登录教学装置迫近段飞行阶段，显示一级火箭、二级火箭均已分离，其中一级火箭已完成回收功能，服务舱为报警状态，报警信息为电压低，其余装置状态正常；如图3C所示为模拟月球登录教学装置月球登录阶段，显示登陆舱已和指令舱与服务舱分离，状态为月球登录中，指令舱与服务舱在月球轨道待命，服务舱为报警状态已解除；如图3D所示为模拟月球登录教学装置返回阶段，显示只有指令舱返回地球，其余装置除一级火箭已回收外均已分离，返航状态正常，无报警信息显示。
需要说明的是，尽管在附图中以特定顺序描述了本公开中方法的各个步骤，但是，这并非要求或者暗示必须按照该特定顺序来执行这些步骤，或是必须执行全部所示的步骤才能实现期望的结果。附加的或备选的，可以省略某些步骤，将多个步骤合并为一个步骤执行，以及/或者将一个步骤分解为多个步骤执行等。
此外，在本示例实施例中，还提供了一种模拟星球登陆的教学装置。参照图4所示，该模拟星球登陆的教学装置400可以包括：信息建立模块410，位置标注模块420，信息对比模块430，状态评分模块440以及结果统计模块450。其中：
信息建立模块410，用于建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；
位置标注模块420，用于动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并提示所述航天器登陆教学信息；
信息对比模块430，用于接收用户的航天器登陆操作信息，将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，以及，将所述航天器登陆操作信息与所述航天器登陆教学信息对比，并得到对比结果；
状态评分模块440，用于根据所述对比结果对用户的模拟操作状态进行评分；
结果统计模块450，用于在确定所述航天器登陆所述待登陆星球后，统计对用户的模拟操作状态的评分结果。
上述中各模拟星球登陆的教学装置模块的具体细节已经在对应的音频段落识别方法中进行了详细的描述，因此此处不再赘述。
应当注意，尽管在上文详细描述中提及了模拟星球登陆的教学装置400的若干模块或者单元，但是这种划分并非强制性的。实际上，根据本公开的实施方式，上文描述的两个或更多模块或者单元的特征和功能可以在一个模块或者单元中具体化。反之，上文描述的一个模块或者单元的特征和功能可以进一步划分为由多个模块或者单元来具体化。
此外，在本公开的示例性实施例中，还提供了一种能够实现上述方法的电子设备。
所属技术领域的技术人员能够理解，本发明的各个方面可以实现为系统、方法或程序产品。因此，本发明的各个方面可以具体实现为以下形式，即：完全的硬件实施例、完全的软件实施例(包括固件、微代码等)，或硬件和软件方面结合的实施例，这里可以统称为“电路”、“模块”或“系统”。
下面参照图5来描述根据本发明的这种实施例的电子设备500。图5显示的电子设备500仅仅是一个示例，不应对本发明实施例的功能和使用范围带来任何限制。
如图5所示，电子设备500以通用计算设备的形式表现。电子设备500的组件可以包括但不限于：上述至少一个处理单元510、上述至少一个存储单元520、连接不同系统组件(包括存储单元520和处理单元510)的总线530、显示单元540。
其中，所述存储单元存储有程序代码，所述程序代码可以被所述处理单元510执行，使得所述处理单元510执行本说明书上述“示例性方法”部分中描述的根据本发明各种示例性实施例的步骤。例如，所述处理单元510可以执行如图1中所示的步骤S110至步骤S150。
存储单元520可以包括易失性存储单元形式的可读介质，例如随机存取存储单元(RAM)5201和/或高速缓存存储单元5202，还可以进一步包括只读存储单元(ROM)5203。
存储单元520还可以包括具有一组(至少一个)程序模块5205的程序/实用工具5204，这样的程序模块5205包括但不限于：操作系统、一个或者多个应用程序、其它程序模块以及程序数据，这些示例中的每一个或某种组合中可能包括网络环境的实现。
总线530可以为表示几类总线结构中的一种或多种，包括存储单元总线或者存储单元控制器、外围总线、图形加速端口、处理单元或者使用多种总线结构中的任意总线结构的局域总线。
电子设备500也可以与一个或多个外部设备570(例如键盘、指向设备、蓝牙设备等)通信，还可与一个或者多个使得用户能与该电子设备500交互的设备通信，和/或与使得该电子设备500能与一个或多个其它计算设备进行通信的任何设备(例如路由器、调制解调器等等)通信。这种通信可以通过输入/输出(I/O)接口550进行。并且，电子设备500还可以通过网络适配器560与一个或者多个网络(例如局域网(LAN)，广域网(WAN)和/或公共网络，例如因特网)通信。如图所示，网络适配器560通过总线530与电子设备500的其它模块通信。应当明白，尽管图中未示出，可以结合电子设备500使用其它硬件和/或软件模块，包括但不限于：微代码、设备驱动器、冗余处理单元、外部磁盘驱动阵列、RAID系统、磁带驱动器以及数据备份存储系统等。
通过以上的实施例的描述，本领域的技术人员易于理解，这里描述的示例实施例可以通过软件实现，也可以通过软件结合必要的硬件的方式来实现。因此，根据本公开实施例的技术方案可以以软件产品的形式体现出 来，该软件产品可以存储在一个非易失性存储介质(可以是CD-ROM，U盘，移动硬盘等)中或网络上，包括若干指令以使得一台计算设备(可以是个人计算机、服务器、终端装置、或者网络设备等)执行根据本公开实施例的方法。
在本公开的示例性实施例中，还提供了一种计算机可读存储介质，其上存储有能够实现本说明书上述方法的程序产品。在一些可能的实施例中，本发明的各个方面还可以实现为一种程序产品的形式，其包括程序代码，当所述程序产品在终端设备上运行时，所述程序代码用于使所述终端设备执行本说明书上述“示例性方法”部分中描述的根据本发明各种示例性实施例的步骤。参考图6所示，描述了根据本发明的实施例的用于实现上述方法的程序产品600，其可以采用便携式紧凑盘只读存储器(CD-ROM)并包括程序代码，并可以在终端设备，例如个人电脑上运行。然而，本发明的程序产品不限于此，在本文件中，可读存储介质可以是任何包含或存储程序的有形介质，该程序可以被指令执行系统、装置或者器件使用或者与其结合使用。
所述程序产品可以采用一个或多个可读介质的任意组合。可读介质可以是可读信号介质或者可读存储介质。可读存储介质例如可以为但不限于电、磁、光、电磁、红外线、或半导体的系统、装置或器件，或者任意以上的组合。可读存储介质的更具体的例子(非穷举的列表)包括：具有一个或多个导线的电连接、便携式盘、硬盘、随机存取存储器(RAM)、只读存储器(ROM)、可擦式可编程只读存储器(EPROM或闪存)、光纤、便携式紧凑盘只读存储器(CD-ROM)、光存储器件、磁存储器件、或者上述的任意合适的组合。
计算机可读信号介质可以包括在基带中或者作为载波一部分传播的数据信号，其中承载了可读程序代码。这种传播的数据信号可以采用多种形式，包括但不限于电磁信号、光信号或上述的任意合适的组合。可读信号介质还可以是可读存储介质以外的任何可读介质，该可读介质可以发送、传播或者传输用于由指令执行系统、装置或者器件使用或者与其结合使用的程序。
可读介质上包含的程序代码可以用任何适当的介质传输，包括但不限于无线、有线、光缆、RF等等，或者上述的任意合适的组合。
可以以一种或多种程序设计语言的任意组合来编写用于执行本发明操作的程序代码，所述程序设计语言包括面向对象的程序设计语言—诸如Java、C++等，还包括常规的过程式程序设计语言—诸如“C”语言或类似的程序设计语言。程序代码可以完全地在用户计算设备上执行、部分地在用户设备上执行、作为一个独立的软件包执行、部分在用户计算设备上部分在远程计算设备上执行、或者完全在远程计算设备或服务器上执行。在涉及远程计算设备的情形中，远程计算设备可以通过任意种类的网络，包括局域网(LAN)或广域网(WAN)，连接到用户计算设备，或者，可以连接到外部计算设备(例如利用因特网服务提供商来通过因特网连接)。
此外，上述附图仅是根据本发明示例性实施例的方法所包括的处理的示意性说明，而不是限制目的。易于理解，上述附图所示的处理并不表明或限制这些处理的时间顺序。另外，也易于理解，这些处理可以是例如在多个模块中同步或异步执行的。
本领域技术人员在考虑说明书及实践这里公开的发明后，将容易想到本公开的其他实施例。本申请旨在涵盖本公开的任何变型、用途或者适应性变化，这些变型、用途或者适应性变化遵循本公开的一般性原理并包括本公开未公开的本技术领域中的公知常识或惯用技术手段。说明书和实施例仅被视为示例性的，本公开的真正范围和精神由权利要求指出。
应当理解的是，本公开并不局限于上面已经描述并在附图中示出的精确结构，并且可以在不脱离其范围进行各种修改和改变。本公开的范围仅由所附的权利要求来限。
工业实用性
一方面，由于真实的模拟了地球至待登陆星球的轨道信息，并给予用户真实的操作感受，可以加深用户对登陆星球过程各阶段轨道的学习；另一方面，通过对航天器状态等教学信息的标注，可以让用户掌握航天器模 拟地球至待登陆星球登陆整个过程中各个技术要点，对所述登陆过程、航天器特性都有比较全面的学习。

Claims (15)

  1. 一种模拟星球登陆的教学方法，其特征在于，所述方法包括以下步骤：
    信息建立步骤：建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；
    位置标注步骤：动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并提示所述航天器登陆教学信息；
    信息对比步骤：接收用户的航天器登陆操作信息，将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，以及，将所述航天器登陆操作信息与所述航天器登陆教学信息对比，并得到对比结果；
    状态评分步骤：根据所述对比结果对用户的模拟操作状态进行评分；
    结果统计步骤：在确定所述航天器登陆所述待登陆星球后，统计对用户的模拟操作状态的评分结果。
  2. 如权利要求1所述的方法，其特征在于，所述状态评分步骤包括：
    第一评分子步骤：判断动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息是否一致，若一致，对用户的模拟操作状态添加加分标识，否则，对用户的模拟操作状态添加减分标识；以及，
    第二评分子步骤：判断所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息是否一致，若一致，对用户的模拟操作状态添加加分标识，否则，对用户的模拟操作状态添加减分标识。
  3. 如权利要求2所述的方法，其特征在于，在判断动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息是否一致后，所述方法还包括：
    若确定动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息不一致，检测两者之间的偏差值；
    根据所述偏差值计算对用户的模拟操作状态的减分分值，并将所述减分分值作为所述减分标识。
  4. 如权利要求2所述的方法，其特征在于，在判断所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息是否一致后，所述方法还包括：
    若确定所述航天器登陆操作信息与所述航天器登陆教学信息中的对应信息一致，检测用户对航天器登陆操作的及时度；
    根据所述及时度计算对用户的模拟操作状态的加分分值，并将所述加分分值作为所述加分标识。
  5. 如权利要求2所述的方法，其特征在于，所述方法还包括，连续加分检测步骤：
    在对用户的模拟操作状态添加加分标识后，检测是否对用户的模拟操作状态连续多次添加加分标识，若是，则增加对用户的模拟操作状态的加分分值，并将增加的加分分值作为额外的加分标识。
  6. 如权利要求1-4任意一项所述的方法，其特征在于，
    所述航天器登陆教学信息包括火箭分离时间信息、航天器驾驶信息、登陆位置选择信息、待登陆星球信息的至少一项。
  7. 如权利要求1-4任意一项所述的方法，其特征在于，
    所述航天器登陆操作信息包括航天器方向操作信息、动力操作信息，航天器姿态信息的至少一项。
  8. 如权利要求1所述的方法，其特征在于，在结果统计步骤之后，所述方法还包括，信息保存步骤：
    将所述评分结果以及从模拟地球至待登陆星球的登陆过程中用户的模拟操作状态作为用户的历史模拟登陆信息并保存。
  9. 如权利要求1或8所述的方法，其特征在于，所述方法还包括，快进操作步骤：
    在检测到当前的航天器登陆模式为重复学习模式时，调取用户的历史模拟登陆信息；
    将用户当前登陆操作阶段与所述历史模拟登陆信息进行匹配，在确定 当前登陆操作阶段为历史模拟登陆信息中的正确操作阶段时，向用户发送是否快进的询问指令；
    在接收到用户回复的确认快进指令后，将所述正确操作阶段的流程进行快进操作。
  10. 如权利要求1所述的方法，其特征在于，所述航天器登陆轨道信息包括上升段轨道信息、迫近段轨道信息和登陆段轨道信息。
  11. 如权利要求1所述的方法，其特征在于，所述方法还包括，状态显示步骤：
    根据航天器的航行时间、航行里程以及预设的航天器燃料信息计算所述航天器的剩余燃料信息；
    获取地球至待登陆星球的剩余里程；
    根据剩余燃料信息以及剩余里程计算剩余可航行时间和/或剩余可航行里程；
    将航行时间、航行里程、剩余燃料信息、剩余里程以及剩余可航行时间和/或剩余可航行里程作为航天器状态，并显示。
  12. 一种模拟星球登陆的教学装置，其特征在于，所述装置包括：
    信息建立模块，用于建立模拟地球至待登陆星球的航天器登陆轨道信息以及航天器登陆教学信息；
    位置标注模块，用于动态标注航天器在模拟地球至待登陆星球的登陆轨道上的位置，并提示所述航天器登陆教学信息；
    信息对比模块，用于接收用户的航天器登陆操作信息，将动态标注的航天器在登陆轨道上的位置与所述航天器登陆轨道信息进行对比，以及，将所述航天器登陆操作信息与所述航天器登陆教学信息对比，并得到对比结果；
    状态评分模块，用于根据所述对比结果对用户的模拟操作状态进行评分；
    结果统计模块，用于在确定所述航天器登陆所述待登陆星球后，统计 对用户的模拟操作状态的评分结果。
  13. 一种电子设备，其特征在于，包括
    处理器；以及
    存储器，所述存储器上存储有计算机可读指令，所述计算机可读指令被所述处理器执行时实现根据权利要求1至11中任一项所述的方法。
  14. 一种计算机程序，包括被加载至计算机系统并被执行时执行根据权利要求1-11中任一项的方法的步骤的计算机程序代码。
  15. 一种计算机可读存储介质，其上存储有包含权利要求14的计算机程序。
PCT/CN2018/092771 2018-03-02 2018-06-26 模拟星球登陆的教学方法以及装置 WO2019165730A1 (zh)

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