CN108550294B - Teaching method and device for simulating planet landing - Google Patents
Teaching method and device for simulating planet landing Download PDFInfo
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Abstract
The disclosure relates to a teaching method and device for simulating planet landing, electronic equipment and a storage medium. Wherein, the method comprises the following steps: establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to a planet to be landed; dynamically marking the position of a spacecraft on a landing orbit from a simulated earth to a planet to be landed, comparing the position with information of the landing orbit of the spacecraft after receiving operation information of the user spacecraft, prompting the spacecraft to land teaching information, and comparing the position with the information of the landing operation of the spacecraft; and grading the simulated operation state of the user according to the comparison result, and counting the grading result of the simulated operation state of the user. The teaching method can realize teaching of simulating the planet landing from the earth to the spacecraft to be landed on the planet.
Description
Technical Field
The disclosure relates to the technical field of computers, in particular to a teaching method and device for simulating planet landing, electronic equipment and a computer readable storage medium.
Background
At present, with the rapid development of human science and technology, the exploration of unknown space in the universe is more and more concerned by people, and particularly, the exploration from the earth to other stars becomes a great dream, so that the problem of teaching how to log in the stars also comes along. The teaching of high-quality planet landing can arouse the interest of people in outer space exploration and can also enhance the understanding of people on other planets in the universe.
However, the existing methods for simulating the planet landing are still only a preliminary exploration phase, generally mainly simulate the space microgravity environment and the game experience, and cannot achieve the teaching purpose. For example:
patent application with application number CN201710159287.6 discloses a dedicated simulation space capsule system of teenager's national defense space education to and disclose the infrastructure in this system, including space capsule, bulkhead protection pad, interior cabin floor, evading cabin, left side propeller, right side propeller, advance the hatch door, advance the rotatory handle of cabin switch etc. its aim at: the simulated space capsule system is used for showing space culture and space science and technology to generate a vivid space simulated environment, so that teenagers can experience space life experience of space weightless state and reverse convolution through simulated space facilities and space capsule environment. The application only discloses hardware facilities of a simulated space capsule system special for teenager space education, and the hardware facilities only can provide microgravity sensory experience for the teenagers in the space environment and cannot achieve the purpose of providing teaching in the process of astroglial landing for users.
The patent application with the application number of CN201210484568.6 discloses a space microgravity simulation experiment system, which mainly comprises a peripheral frame, a leveling system, a passive adjusting mechanism in a horizontal plane, a Z-direction active gravity compensation system, a rotation passive adjusting mechanism and a pitching deflection active adjusting system, and the space microgravity environment is simulated through the cooperation of all the parts, so that the posture change of an experimental object is completed, and the zero gravity state is reproduced.
Patent application with application number CN03276220.8 discloses a simulation spacecraft, through computer centralized control, according to the process of space flight, "outside the window" sight, the sound of TV set broadcast, with the utility model discloses a collision, vibrations to and the flight angle in flight storehouse 2, the interior temperature of storehouse coincide unanimously, make the visitor feel realistically and receive space flight's experience, experience multiple space flight actions such as slope, turn round, collision, rock, rotation.
The 'recreation spaceship' with application number of CN92200996.1 utilizes universal connecting shafts and lifters and the like to enable people to meet the simulation requirements of inviting space in the aspects of motion feeling, environment feeling and observation feeling.
The magnetic suspension space amusement ship with the application number of CN00234436.X utilizes the high-strength magnet at the bottom of the ship and the high-strength magnet on the running slideway to enable the amusement ship to be in a suspension state, and when tourists in the amusement ship naturally slide down along a high slope, space swimming inviting feeling is generated.
In the prior art, the simulation of the space microgravity environment or the space game experience of the user is only carried out by simply simulating the spacecraft, and the following problems still exist in relation to the teaching in the process of simulating the planet landing:
technical points and evaluation in the process of simulating the earth to land on the planet to be landed by a spacecraft cannot be provided for a user, learning in the process of simulating the planet landing by an astronaut cannot be completed, and the aim of teaching the planet landing cannot be fulfilled.
The space landing teaching method aims at the problems in the prior art, and mainly aims to enable a user to simulate a planet landing process and learn courses in the aspect of space teaching on the basis of space experience in a space microgravity environment simulation, so that the purpose of planet landing teaching is achieved.
It is to be noted that the information disclosed in the above background section is only for enhancement of understanding of the background of the present disclosure, and thus may include information that does not constitute prior art known to those of ordinary skill in the art.
Disclosure of Invention
The invention aims to provide a teaching method, a device, electronic equipment and a computer readable storage medium for simulating planet landing, and aims to solve the operation learning such as experience, teaching and evaluation in the teaching of the spacecraft landing from the simulated earth to the planet to be landed, so that a user can master all technical points in the whole process from the simulated earth to the planet to be landed landing, and particularly has relatively comprehensive learning on the landing process and the spacecraft characteristics. The improvements of the invention include the following:
the method comprises the steps of dynamically marking the position of a spacecraft on a landing orbit from a simulated earth to a planet to be landed by pre-establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to the planet to be landed, comparing with the spacecraft landing orbit information after receiving user spacecraft operation information, prompting the spacecraft to land the teaching information, comparing with the spacecraft landing operation information, grading the simulated operation state of a user according to the comparison result, counting the grading result of the simulated operation state of the user, truly simulating the orbit information from the earth to the planet to be landed, giving the user a real operation feeling, deepening the learning of the user on the orbit in each stage of a planet landing process, enabling the user to master various technical points in the whole process from the simulation of the spacecraft to the planet to be landed, and enabling the user to master various technical points in the whole process from the simulation of the earth to the planet to be landed, The characteristics of the spacecraft can be comprehensively learned.
Different execution instructions and actions are set in different orbit sections of the spacecraft, so that landing teaching information of the spacecraft corresponding to the different orbit sections is different, for example, when the orbit is in an ascending section, the separation of a multi-stage rocket, the separation of an escape tower and the like are monitored, when the orbit is in an approaching section, the orbit and the attitude of the spacecraft are required to be adjusted for many times, when the orbit is in a landing section, the information of a planet to be landed and landing position information are required to be known, and the control or detection of other states in the whole landing process of the spacecraft is required. The method can help the user to learn the whole process of the spacecraft landing the planet to be landed more deeply, strengthen the intuitive learning of the landing teaching information of the spacecraft, and play a teaching effect with half the effort.
After judging whether the spacecraft login operation information is consistent with the corresponding information in the spacecraft login teaching information or not, detecting the timeliness of the user on the spacecraft login operation when the spacecraft login operation information is determined to be consistent with the corresponding information in the spacecraft login teaching information, calculating the score of the simulated operation state of the user according to the timeliness, and further measuring the accuracy of the spacecraft login operation information.
The bonus mark is added to the simulated operation state of the user, and after the fact that the bonus mark is continuously added to the simulated operation state of the user for multiple times is detected, the bonus mark of the simulated operation state of the user can be added, and the added bonus mark is used as an additional bonus mark. The method and the device for enhancing the teaching experience have the advantage that the correct behavior of the user continuous simulation operation is awarded in a point adding mode, and therefore the learning interest of the user is improved.
After the scoring result of the simulated operation state of the user is counted, the scoring result and the simulated operation state of the user in the login process from the simulated earth to the planet to be logged in are used as historical simulated login information of the user and stored. And recording the scoring result of each user logging in the planet to be logged each time so as to be used for overall data statistics or review and review of the user in the future.
According to one aspect of the present disclosure, a teaching method for simulating a planet landing is provided, which includes the following steps:
an information establishing step: establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to a planet to be landed;
position marking: dynamically marking the position of a spacecraft on a landing orbit from a simulated earth to a planet to be landed, and prompting the spacecraft to land teaching information;
and information comparison step: receiving spacecraft landing operation information of a user, comparing the position of a dynamically marked spacecraft on a landing track with the spacecraft landing track information, and comparing the spacecraft landing operation information with the spacecraft landing teaching information to obtain a comparison result;
and (3) state scoring: grading the simulated operation state of the user according to the comparison result;
and (5) counting results: and after the spacecraft is confirmed to log in the to-be-logged planet, counting the scoring result of the simulated operation state of the user.
In an exemplary embodiment of the present disclosure, scoring the simulated operation state of the user according to the comparison result includes:
a first scoring substep: judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the information of the landing orbit of the spacecraft, if so, adding a mark adding identifier to the simulated operation state of the user, otherwise, adding a mark subtracting identifier to the simulated operation state of the user; and the number of the first and second groups,
a second scoring substep: and judging whether the spacecraft login operation information is consistent with corresponding information in the spacecraft login teaching information, if so, adding a mark for adding marks to the simulated operation state of the user, and otherwise, adding a mark for subtracting marks to the simulated operation state of the user.
In an exemplary embodiment of the present disclosure, after determining whether a position of a dynamically labeled spacecraft on a landing orbit is consistent with the spacecraft landing orbit information, the method further includes:
if the position of the dynamically marked spacecraft on the landing orbit is determined to be inconsistent with the information of the landing orbit of the spacecraft, detecting a deviation value between the position of the dynamically marked spacecraft on the landing orbit and the landing orbit;
and calculating a score reduction value of the simulation operation state of the user according to the deviation value, and taking the score reduction value as the score reduction identification.
In an exemplary embodiment of the present disclosure, after determining whether the spacecraft login operation information is consistent with corresponding information in the spacecraft login teaching information, the method further includes a timeliness detection step:
if the spacecraft landing operation information is determined to be consistent with the corresponding information in the spacecraft landing teaching information, detecting the timeliness of a user for the spacecraft landing operation;
and calculating a scoring value of the simulation operation state of the user according to the timeliness, and taking the scoring value as the scoring identifier.
In an exemplary embodiment of the present disclosure, the method further includes, a continuous bonus detecting step of:
after adding the bonus mark to the simulation operation state of the user, detecting whether the bonus mark is continuously added to the simulation operation state of the user for multiple times, if so, increasing the bonus mark to the simulation operation state of the user, and taking the increased bonus mark as an additional bonus mark.
In an exemplary embodiment of the present disclosure, the spacecraft landing teaching information includes at least one of rocket separation time information, spacecraft driving information, landing position selection information, and information of a planet to be landed.
In an exemplary embodiment of the present disclosure, the spacecraft landing operation information includes at least one of spacecraft directional operation information, power operation information, and spacecraft attitude information.
In an exemplary embodiment of the present disclosure, after counting a scoring result of a simulated operation state of a user, the method further includes an information saving step of:
and taking the scoring result and the simulated operation state of the user in the login process from the simulated earth to the planet to be logged in as historical simulated login information of the user and storing the historical simulated login information.
In an exemplary embodiment of the present disclosure, the method further includes a fast forward operation step of:
when the current spacecraft login mode is detected to be the repeated learning mode, calling historical simulation login information of a user;
matching the current login operation stage of the user with the historical simulation login information, and sending an inquiry instruction for judging whether to fast forward to the user when the current login operation stage is determined to be the correct operation stage in the historical simulation login information;
and after receiving a fast forward confirmation instruction replied by the user, carrying out fast forward operation on the flow of the correct operation stage.
In an exemplary embodiment of the present disclosure, the spacecraft landing orbit information includes ascending segment orbit information, approaching segment orbit information, and landing segment orbit information.
In an exemplary embodiment of the present disclosure, the method further includes a status display step of:
calculating the residual fuel information of the spacecraft according to the navigation time and the navigation mileage of the spacecraft and the preset fuel information of the spacecraft;
acquiring the remaining mileage from the earth to a planet to be landed;
calculating the remaining navigable time and/or the remaining navigable mileage according to the remaining fuel information and the remaining mileage;
and taking the sailing time, the sailing mileage, the remaining fuel information, the remaining mileage and the remaining navigable time and/or the remaining navigable mileage as the states of the spacecraft and displaying the states.
In one aspect of the present disclosure, there is provided a teaching device for simulating a planet landing, comprising:
the information establishing module is used for establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to a planet to be landed;
the position marking module is used for dynamically marking the position of the spacecraft on a landing orbit from the simulated earth to a planet to be landed and prompting the spacecraft to land teaching information;
the information comparison module is used for receiving spacecraft landing operation information of a user, comparing the position of the dynamically marked spacecraft on a landing track with the spacecraft landing track information, comparing the spacecraft landing operation information with the spacecraft landing teaching information and obtaining a comparison result;
the state scoring module is used for scoring the simulation operation state of the user according to the comparison result;
and the result counting module is used for counting the scoring result of the simulation operation state of the user after the spacecraft is determined to log in the planet to be logged.
In one aspect of the present disclosure, there is provided an electronic device including:
a processor; and
a memory having computer readable instructions stored thereon which, when executed by the processor, implement a method according to any of the above.
In an aspect of the disclosure, a computer-readable storage medium is provided, on which a computer program is stored, which computer program, when being executed by a processor, realizes the method according to any one of the above.
The teaching method for simulating the planet landing in the exemplary embodiment of the disclosure establishes spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to the planet to be landed; dynamically marking the position of a spacecraft on a landing orbit from a simulated earth to a planet to be landed, comparing the position with information of the landing orbit of the spacecraft after receiving operation information of the user spacecraft, prompting the spacecraft to land teaching information, and comparing the position with the information of the landing operation of the spacecraft; and grading the simulated operation state of the user according to the comparison result, and counting the grading result of the simulated operation state of the user. On one hand, the orbit information from the earth to the planet to be landed is truly simulated, and the user is given a real operation feeling, so that the learning of the user on the orbit at each stage in the process of landing the planet can be deepened; on the other hand, by marking teaching information such as the state of the spacecraft and the like, a user can master all technical points of the whole process from the simulation of the spacecraft to the planet to be landed to land, and the landing process and the characteristics of the spacecraft can be comprehensively learned.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the disclosure.
Drawings
The above and other features and advantages of the present disclosure will become more apparent by describing in detail exemplary embodiments thereof with reference to the attached drawings.
FIG. 1 shows a flow chart of a teaching method of simulating a star landing according to an exemplary embodiment of the present disclosure;
2A-2B show schematic diagrams of teaching devices simulating a star landing according to an exemplary embodiment of the present disclosure;
3A-3D show schematic diagrams of a teaching device for simulating planet landing showing the state of a spacecraft at various stages of simulating planet landing according to an exemplary embodiment of the present disclosure;
FIG. 4 shows a schematic block diagram of a teaching device simulating a planet landing according to an exemplary embodiment of the present disclosure;
FIG. 5 schematically illustrates a block diagram of an electronic device according to an exemplary embodiment of the present disclosure; and
fig. 6 schematically illustrates a schematic diagram of a computer-readable storage medium according to an exemplary embodiment of the present disclosure.
Detailed Description
Example embodiments will now be described more fully with reference to the accompanying drawings. Example embodiments may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the concept of example embodiments to those skilled in the art. The same reference numerals denote the same or similar parts in the drawings, and thus, a repetitive description thereof will be omitted.
Furthermore, the described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. In the following description, numerous specific details are provided to give a thorough understanding of embodiments of the disclosure. One skilled in the relevant art will recognize, however, that the embodiments of the disclosure can be practiced without one or more of the specific details, or with other methods, components, materials, devices, steps, and so forth. In other instances, well-known structures, methods, devices, implementations, materials, or operations are not shown or described in detail to avoid obscuring aspects of the disclosure.
The block diagrams shown in the figures are functional entities only and do not necessarily correspond to physically separate entities. That is, these functional entities may be implemented in the form of software, or in one or more software-hardened modules, or in different networks and/or processor devices and/or microcontroller devices.
In the embodiment, firstly, a teaching method for simulating planet landing is provided, which can be applied to electronic equipment such as a computer; referring to fig. 1, the teaching method for simulating planet landing may include the following steps:
information creation step S110: establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to a planet to be landed;
position labeling step S120: dynamically marking the position of a spacecraft on a landing orbit from a simulated earth to a planet to be landed, and prompting the spacecraft to land teaching information;
information comparison step S130: receiving spacecraft landing operation information of a user, comparing the position of a dynamically marked spacecraft on a landing track with the spacecraft landing track information, and comparing the spacecraft landing operation information with the spacecraft landing teaching information to obtain a comparison result;
state scoring step S140: grading the simulated operation state of the user according to the comparison result;
result statistics step S150: and after the spacecraft is confirmed to log in the to-be-logged planet, counting the scoring result of the simulated operation state of the user.
According to the teaching method for simulating the planet landing in the embodiment, on one hand, the orbit information from the earth to the planet to be landed is really simulated, and the user is given real operation feeling, so that the learning of the user on the orbit of each stage in the planet landing process can be deepened; on the other hand, by marking teaching information such as the state of the spacecraft and the like, a user can master all technical points of the whole process from the simulation of the spacecraft to the planet to be landed to land, and the landing process and the characteristics of the spacecraft can be comprehensively learned.
Next, a teaching method of simulating a star landing in the present exemplary embodiment will be further described.
In the information establishing step S110, spacecraft landing orbit information and spacecraft landing teaching information for simulating that the earth lands on the celestial sphere to be landed can be established;
in this exemplary embodiment, to perform teaching of a spacecraft simulation landing planet, first, information of a spacecraft landing orbit from a simulated earth to a to-be-landed planet is established, where the to-be-landed planet may be a planet that has been explored, such as moon, mars, hallout comet, and the like, or a planet of virtual data that is established for teaching practice. The spacecraft landing orbit information refers to all orbit information of all parts of the spacecraft launched from the earth until landing of a to-be-landed planet is successfully simulated.
Different instructions can be executed in the process that the spacecraft simulates the earth to land on the planet to be landed, different actions are completed, the spacecraft can land successfully, the instructions and the actions can be spacecraft landing teaching information, and a user can learn to experience the whole process that the spacecraft simulates the landing.
In this example embodiment, the spacecraft landing orbit information includes ascending segment orbit information, approaching segment orbit information, and landing segment orbit information. The spacecraft landing orbit information comprises ascending section orbit information of a spacecraft launched from the earth to the earth orbit, approach section orbit information of the spacecraft launched from the earth orbit to the planet orbit to be landed, and landing section orbit information of the spacecraft launched from the planet orbit to be landed to the surface of the planet to be landed. When the landing distance is long, or the approach mode is complex, such as the need of surrounding a third planet for multiple times, or the planet to be landed by utilizing the gravity slingshot, the approach section track information can be the combination of a plurality of approach section track information.
In this exemplary embodiment, the spacecraft landing teaching information includes at least one of rocket separation time information, spacecraft driving information, landing position selection information, and information of a celestial sphere to be landed. The instructions and actions executed in different orbit sections of the spacecraft are different, corresponding teaching information for landing of the spacecraft is also different, for example, when the orbit is in an ascending section, the separation of a multi-stage rocket and the separation of an escape tower need to be monitored, when the orbit is in an approaching section, the orbit and the attitude of the spacecraft need to be adjusted for many times, when the orbit is in a landing section, the information of a planet to be landed and landing position information need to be known, and the control or detection of other states in the whole landing process of the spacecraft, such as the residual fuel quantity, the state of a life support system, the communication state, the angle of an antenna and the like, are required. The information can help the user to learn the whole process of the spacecraft landing the planet to be landed more deeply, the intuitive learning of the spacecraft landing teaching information is enhanced, and the teaching effect of getting twice with half the effort can be achieved.
In the position marking step S120, the position of the spacecraft on the landing orbit from the simulated earth to the celestial sphere to be landed can be dynamically marked, and the spacecraft is prompted to land teaching information;
in this exemplary embodiment, as shown in fig. 2A and 2B, a schematic display interface of a teaching system for a spacecraft to simulate the earth to a planet to be landed is shown, where the schematic display interface includes a position of the spacecraft, which is dynamically marked and displayed, on a landing orbit of the simulated earth to the planet to be landed, and the position dynamically changes along with direction operations of a user, such as a departure from the orbit, and an alarm prompt is given, and the teaching system further includes teaching information for the spacecraft to land, so that the user can quickly know currently recommended direction operations and the like and other teaching content information. As shown in fig. 2A, in a schematic display interface of a spacecraft simulated earth to a to-be-landed celestial sphere teaching system, spacecraft orbit position information is normal, and no direction operation prompt is given; as shown in fig. 2B, the spacecraft deviates from the login orbit in a schematic display interface of the to-be-logged celestial sphere teaching system simulated by the spacecraft, and the spacecraft displays prompt direction operation information on the display interface of the to-be-logged celestial sphere teaching system simulated by the spacecraft.
In the information comparison step S130, spacecraft landing operation information of the user may be received, the dynamically labeled position of the spacecraft on the landing orbit is compared with the spacecraft landing orbit information, and the spacecraft landing operation information is compared with the spacecraft landing teaching information to obtain a comparison result;
in the embodiment, after receiving spacecraft landing operation information of a user, mainly direction operation information of the user, the direction operation information is generated into corresponding displacement to be displayed on a landing orbit of a spacecraft, then the position of the dynamically marked spacecraft on the landing orbit is compared with the spacecraft landing orbit information, and a difference value between a theoretical position and an actual position is compared. Meanwhile, after receiving spacecraft landing operation information of a user, mainly state or control operation information, comparing the state or control operation with the spacecraft landing teaching information.
In this example embodiment, 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 comprises spacecraft direction operation information for controlling the direction of a spacecraft, power operation information for controlling the speed of the spacecraft, spacecraft attitude information for controlling the attitude of the spacecraft and the like. Further, rocket separation information, spacecraft docking information and the like are included.
In the state scoring step S140, 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 substep S1401 and a second scoring substep S1402.
First scoring substep S1401: judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the information of the landing orbit of the spacecraft, if so, adding a mark adding identifier to the simulated operation state of the user, otherwise, adding a mark subtracting identifier to the simulated operation state of the user; and the number of the first and second groups,
second scoring substep S1402: and judging whether the spacecraft login operation information is consistent with corresponding information in the spacecraft login teaching information, if so, adding a mark for adding marks to the simulated operation state of the user, and otherwise, adding a mark for subtracting marks to the simulated operation state of the user.
In this example embodiment, scoring the simulated operation state of the user according to the comparison result is one of the methods for evaluating the teaching result, so that the learning and mastering degree of the user can be quickly known, and the learning interest of the user can be improved. Different scores can be set according to the difficulty of the spacecraft in logging in the teaching information. Meanwhile, the score adding mark or the score subtracting mark can be divided into zero scores, that is, all users can add scores and not deduct scores or only deduct scores and not add scores uniformly.
In this exemplary embodiment, the method further includes a continuous bonus detecting step: after adding the bonus mark to the simulation operation state of the user, detecting whether the bonus mark is continuously added to the simulation operation state of the user for multiple times, if so, increasing the bonus mark to the simulation operation state of the user, and taking the increased bonus mark as an additional bonus mark. In order to enhance the teaching experience, the method can be used for bonus awarding the behaviors of correct continuous simulation operation of the user, and the learning interest of the user is improved.
In this example embodiment, after determining whether the position of the dynamically labeled spacecraft on the landing orbit is consistent with the spacecraft landing orbit information, the method further includes: if the position of the dynamically marked spacecraft on the landing orbit is determined to be inconsistent with the information of the landing orbit of the spacecraft, detecting a deviation value between the position of the dynamically marked spacecraft on the landing orbit and the landing orbit; and calculating a score reduction value of the simulation operation state of the user according to the deviation value, and taking the score reduction value as the score reduction identification. Different scores can be set according to the difficulty degree of the spacecraft landing teaching information, meanwhile, different spacecraft landing operation information corresponding to the same spacecraft landing teaching information are different in implementation degree, grade differences can also be set, and the accuracy degree of the spacecraft landing operation information is reflected. Specifically, a deviation value between the position of the spacecraft on the landing orbit and the information of the landing orbit of the spacecraft can be detected, and the accuracy of the operation information of the landing direction of the spacecraft is measured by the deviation value.
In this example embodiment, after determining whether the spacecraft login operation information is consistent with corresponding information in the spacecraft login teaching information, the method further includes: if the spacecraft landing operation information is determined to be consistent with the corresponding information in the spacecraft landing teaching information, detecting the timeliness of a user for the spacecraft landing operation; and calculating a scoring value of the simulation operation state of the user according to the timeliness, and taking the scoring value as the scoring identifier. The timeliness of the user for the spacecraft login operation can be detected, and the accuracy of the spacecraft login operation information is measured according to the timeliness. Furthermore, the method also comprises the steps of detecting the sequence and the coordination degree of the user for the landing operation of the plurality of spacecrafts, and measuring the accuracy degree of the information of the landing operation of the spacecrafts.
In the result counting step S150, after it is determined that the spacecraft logs in the to-be-logged planet, a scoring result of the simulated operation state of the user may be counted.
In this exemplary embodiment, the total score is calculated according to the scores of the landing operation information of each spacecraft, and the level of the user in the process from the simulated earth to the planet to be landed at this time is measured according to the total score. Meanwhile, if the user completes the login of the planet to be logged in for the first time, the planet to be logged in is marked as the logged-in planet of the user.
In this example embodiment, the method may further include scoring that the user has failed to log in to the planet to be logged due to a faulty operation. And after successfully logging in the planet to be logged in, simulating the scoring of the operation of returning to the earth process from the planet to be logged in.
In this exemplary embodiment, after counting the scoring result of the simulated operation state of the user, the method further includes: and taking the scoring result and the simulated operation state of the user in the login process from the simulated earth to the planet to be logged in as historical simulated login information of the user and storing the historical simulated login information. And recording the scoring result of each user logging in the planet to be logged each time so as to be used for overall data statistics or review and review of the user in the future.
In this example embodiment, the method further comprises: when the current spacecraft login mode is detected to be the repeated learning mode, calling historical simulation login information of a user; matching the current login operation stage of the user with the historical simulation login information, and sending an inquiry instruction for judging whether to fast forward to the user when the current login operation stage is determined to be the correct operation stage in the historical simulation login information; and after receiving a fast forward confirmation instruction replied by the user, carrying out fast forward operation on the flow of the correct operation stage. The teaching method for simulating the landing of the earth on the planet to be landed can have a review function, so that a user can quickly call historical simulated landing information, historical error operation information can be marked in the information specially, review operation can be performed on the historical error operation information emphatically, and fast-forward instructions can be provided for other operation information, so that fast-forward operation can be performed on the flow of the correct operation stage which does not need to be reviewed.
In this example embodiment, the method further comprises: calculating the residual fuel information of the spacecraft according to the navigation time and the navigation mileage of the spacecraft and the preset fuel information of the spacecraft; acquiring the remaining mileage from the earth to a planet to be landed; calculating the remaining navigable time and/or the remaining navigable mileage according to the remaining fuel information and the remaining mileage; and taking the sailing time, the sailing mileage, the remaining fuel information, the remaining mileage and the remaining navigable time and/or the remaining navigable mileage as the states of the spacecraft and displaying the states. The spacecraft state display interface can statically display the navigation time, the navigation mileage and the spacecraft fuel information of the spacecraft, and can display a warning mark when the residual fuel is not enough to complete the next task. In order to enhance the teaching experience of the spacecraft of the user in the process of simulating the landing of the earth on the planet to be landed, the display can also be in a three-dimensional animation mode. As shown in fig. 3A, the simulated moon logs in the to-take-off stage of the teaching device, the first-stage rocket is in an ignition countdown state, the other devices are in normal states, and no alarm information is displayed; as shown in fig. 3B, the simulation of the moon logging in the approaching flight stage of the teaching device shows that the first-stage rocket and the second-stage rocket are both separated, wherein the first-stage rocket finishes the recovery function, the service bay is in the alarm state, the alarm information is low in voltage, and the rest devices are in normal states; as shown in fig. 3C, the simulated lunar logging teaching device comprises a lunar logging phase, which displays that the logging cabin is separated from the command cabin and the service cabin, and the state is that the command cabin and the service cabin are standby on a lunar orbit during lunar logging, and the alarm state of the service cabin is released; as shown in fig. 3D, the simulated moon logs in the teaching device to return, and shows that only the command cabin returns to the earth, the rest devices are separated except for the first-stage rocket which is recovered, the return state is normal, and no alarm information is displayed.
It should be noted that although the various steps of the methods of the present disclosure are depicted in the drawings in a particular order, this does not require or imply that these steps must be performed in this particular order, or that all of the depicted steps must be performed, to achieve desirable results. Additionally or alternatively, certain steps may be omitted, multiple steps combined into one step execution, and/or one step broken down into multiple step executions, etc.
In addition, in the exemplary embodiment, a teaching device for simulating planet landing is also provided. Referring to fig. 4, the teaching device 400 for simulating planet landing may include: the system comprises an information establishing module 410, a position labeling module 420, an information comparing module 430, a state scoring module 440 and a result counting module 450. Wherein:
the information establishing module 410 is used for establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to a planet to be landed;
the position marking module 420 is used for dynamically marking the position of the spacecraft on a landing orbit from the simulated earth to a planet to be landed and prompting the spacecraft to land teaching information;
the information comparison module 430 is configured to receive spacecraft landing operation information of a user, compare the dynamically labeled position of the spacecraft on a landing orbit with the spacecraft landing orbit information, compare the spacecraft landing operation information with the spacecraft landing teaching information, and obtain a comparison result;
the state scoring module 440 is used for scoring the simulation operation state of the user according to the comparison result;
and the result counting module 450 is configured to count a scoring result of the simulated operation state of the user after the spacecraft is determined to log in the to-be-logged planet.
The specific details of each teaching device module simulating the planet landing have been described in detail in the corresponding audio paragraph identification method, and therefore are not described herein again.
It should be noted that although several modules or units of teaching apparatus 400 simulating a star landing are mentioned in the above detailed description, such a division is not mandatory. Indeed, the features and functionality of two or more modules or units described above may be embodied in one module or unit, according to embodiments of the present disclosure. Conversely, the features and functions of one module or unit described above may be further divided into embodiments by a plurality of modules or units.
In addition, in an exemplary embodiment of the present disclosure, an electronic device capable of implementing the above method is also provided.
As will be appreciated by one skilled in the art, aspects of the present invention may be embodied as a system, method or program product. Thus, various aspects of the invention may be embodied in the form of: an entirely hardware embodiment, an entirely software embodiment (including firmware, microcode, etc.) or an embodiment combining hardware and software aspects that may all generally be referred to herein as a "circuit," module "or" system.
An electronic device 500 according to such an embodiment of the invention is described below with reference to fig. 5. The electronic device 500 shown in fig. 5 is only an example and should not bring any limitation to the functions and the scope of use of the embodiments of the present invention.
As shown in fig. 5, the 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 memory unit 520, a bus 530 connecting various system components (including the memory unit 520 and the processing unit 510), and a display unit 540.
Wherein the storage unit stores program code that is executable by the processing unit 510 to cause the processing unit 510 to perform steps according to various exemplary embodiments of the present invention as described in the above section "exemplary methods" of the present specification. For example, the processing unit 510 may perform steps S110 to S150 as shown in fig. 1.
The memory unit 520 may include a readable medium in the form of a volatile memory unit, such as a random access memory unit (RAM)5201 and/or a cache memory unit 5202, and may further include a read only memory unit (ROM) 5203.
The electronic device 500 may also communicate with one or more external devices 570 (e.g., keyboard, pointing device, Bluetooth device, etc.), with one or more devices that enable a user to interact with the electronic device 500, and/or with any devices (e.g., router, modem, etc.) that enable the electronic device 500 to communicate with one or more other computing devices. Such communication may occur via input/output (I/O) interfaces 550. Also, the electronic device 500 may 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 the network adapter 560. As shown, the network adapter 560 communicates with the other modules of the electronic device 500 over the bus 530. It should be appreciated that although not shown in the figures, other hardware and/or software modules may be used in conjunction with the electronic device 500, including but not limited to: microcode, device drivers, redundant processing units, external disk drive arrays, RAID systems, tape drives, and data backup storage systems, among others.
Through the above description of the embodiments, those skilled in the art will readily understand that the exemplary embodiments described herein may be implemented by software, or by software in combination with necessary hardware. Therefore, the technical solution according to the embodiments 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 disk, a removable hard disk, etc.) or on a network, and includes several instructions to enable a computing device (which may be a personal computer, a server, a terminal device, or a network device, etc.) to execute the method according to the embodiments of the present disclosure.
In an exemplary embodiment of the present disclosure, there is also provided a computer-readable storage medium having stored thereon a program product capable of implementing the above-described method of the present specification. In some possible embodiments, aspects of the invention may also be implemented in the form of a program product comprising program code means for causing a terminal device to carry out the steps according to various exemplary embodiments of the invention described in the above-mentioned "exemplary methods" section of the present description, when said program product is run on the terminal device. Referring to fig. 6, a program product 600 for implementing the above method according to an embodiment of the present invention is described, which may employ a portable compact disc read only memory (CD-ROM) and include program code, and may be run on a terminal device, such as a personal computer. However, the program product of the present invention is not limited in this regard and, in the present document, a readable storage medium may be any tangible medium that can contain, or store a program for use by or in connection with an instruction execution system, apparatus, or device.
The program product may employ any combination of one or more readable media. The readable medium may be a readable signal medium or a readable storage medium. A readable storage medium may be, for example, but not limited to, an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any combination of the foregoing. More specific examples (a non-exhaustive list) of the readable storage medium include: an electrical connection having one or more wires, a portable disk, a hard disk, a Random Access Memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or flash memory), an optical fiber, a portable compact disc read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the foregoing.
A computer readable signal medium may include a propagated data signal with readable program code embodied therein, for example, in baseband or as part of a carrier wave. Such a propagated data signal may take many forms, including, but not limited to, electro-magnetic, optical, or any suitable combination thereof. A readable signal medium may also be any readable medium that is not a readable storage medium and that can communicate, 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 may be transmitted using any appropriate medium, including but not limited to wireless, wireline, optical fiber cable, RF, etc., or any suitable combination of the foregoing.
Program code for carrying out operations for aspects 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 + + or the like and conventional procedural programming languages, such as the "C" programming language or similar programming languages. The program code may execute entirely on the user's computing device, partly on the user's device, as a stand-alone software package, partly on the user's computing device and partly on a remote computing device, or entirely on the remote computing device or server. In the case of a remote computing device, the remote computing device may be connected to the user computing device through any kind of network, including a Local Area Network (LAN) or a Wide Area Network (WAN), or may be connected to an external computing device (e.g., through the internet using an internet service provider).
Furthermore, the above-described figures are merely schematic illustrations of processes involved in methods according to exemplary embodiments of the invention, and are not intended to be limiting. It will be readily understood that the processes shown in the above figures are not intended to indicate or limit the chronological order of the processes. In addition, it is also readily understood that these processes may be performed synchronously or asynchronously, e.g., in multiple modules.
Other embodiments of the disclosure will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure disclosed herein. This application is intended to cover any variations, uses, or adaptations of the disclosure following, in general, the principles of the disclosure and including such departures from the present disclosure as come within known or customary practice within the art to which the disclosure pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the disclosure being indicated by the following claims.
It will be understood that the present disclosure is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the present disclosure is to be limited only by the terms of the appended claims.
Claims (8)
1. A teaching method for simulating planet landing is characterized by comprising the following steps:
an information establishing step: establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to a to-be-landed planet, wherein the spacecraft landing teaching information comprises at least one item of rocket separation time information, spacecraft driving information, landing position selection information and to-be-landed planet information;
position marking: dynamically marking the position of a spacecraft on a landing orbit from a simulated earth to a planet to be landed, and prompting the spacecraft to land teaching information;
and information comparison step: receiving spacecraft landing operation information of a user, comparing the position of a dynamically marked spacecraft on a landing track with the spacecraft landing track information, comparing the spacecraft landing operation information with spacecraft landing teaching information, and obtaining a comparison result, wherein the spacecraft landing operation information comprises at least one of spacecraft direction operation information, power operation information and spacecraft attitude information;
and (3) state scoring: grading the simulated operation state of the user according to the comparison result; the state scoring step further comprises: a first scoring substep: judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the information of the landing orbit of the spacecraft, if so, adding a mark adding identifier to the simulated operation state of the user, otherwise, adding a mark subtracting identifier to the simulated operation state of the user; and, a second scoring substep: judging whether the spacecraft login operation information is consistent with corresponding information in the spacecraft login teaching information, if so, adding a mark for adding marks to the simulated operation state of the user, and otherwise, adding a mark for subtracting marks to the simulated operation state of the user;
after judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the information of the landing orbit of the spacecraft, the method further comprises the following steps: if the position of the dynamically marked spacecraft on the landing orbit is determined to be inconsistent with the information of the landing orbit of the spacecraft, detecting a deviation value between the position of the dynamically marked spacecraft on the landing orbit and the landing orbit; calculating a score reduction value of the simulation operation state of the user according to the deviation value, and taking the score reduction value as the score reduction identification;
after judging whether the spacecraft login operation information is consistent with the corresponding information in the spacecraft login teaching information, the method further comprises the following steps: if the spacecraft landing operation information is determined to be consistent with the corresponding information in the spacecraft landing teaching information, detecting the timeliness of a user for the spacecraft landing operation; calculating a scoring value of the simulation operation state of the user according to the timeliness, and taking the scoring value as the scoring identifier;
and (3) continuous adding and detecting steps: after adding the bonus mark to the simulated operation state of the user, detecting whether the bonus mark is continuously added to the simulated operation state of the user for multiple times, if so, increasing the bonus mark to the simulated operation state of the user, and taking the increased bonus mark as an additional bonus mark;
and (5) counting results: after the spacecraft is confirmed to log in the planet to be logged in, counting a scoring result of the simulation operation state of the user;
and a state display step: calculating the residual fuel information of the spacecraft according to the navigation time and the navigation mileage of the spacecraft and the preset fuel information of the spacecraft; acquiring the remaining mileage from the earth to a planet to be landed; calculating the remaining navigable time and/or the remaining navigable mileage according to the remaining fuel information and the remaining mileage; and taking the navigation time, the navigation mileage, the residual fuel information, the residual mileage and the residual navigable time and/or the residual navigable mileage as the states of the spacecraft and displaying the states.
2. The method of claim 1, wherein after the result statistics step, the method further comprises an information saving step of:
and taking the scoring result and the simulated operation state of the user in the login process from the simulated earth to the planet to be logged in as historical simulated login information of the user and storing the historical simulated login information.
3. The method of claim 1, wherein the method further comprises the step of fast forwarding:
when the current spacecraft login mode is detected to be the repeated learning mode, calling historical simulation login information of a user;
matching the current login operation stage of the user with the historical simulation login information, and sending an inquiry instruction for judging whether to fast forward to the user when the current login operation stage is determined to be the correct operation stage in the historical simulation login information;
and after receiving a fast forward confirmation instruction replied by the user, carrying out fast forward operation on the flow of the correct operation stage.
4. The method of claim 1, wherein the spacecraft landing orbit information comprises ascending segment orbit information, approaching segment orbit information, and landing segment orbit information.
5. A teaching device for simulating a star landing, the device comprising:
the information establishing module is used for establishing spacecraft landing orbit information and spacecraft landing teaching information for simulating the earth to a to-be-landed planet, wherein the spacecraft landing teaching information comprises at least one of rocket separation time information, spacecraft driving information, landing position selection information and to-be-landed planet information;
the position marking module is used for dynamically marking the position of the spacecraft on a landing orbit from the simulated earth to a planet to be landed and prompting the spacecraft to land teaching information;
the information comparison module is used for receiving spacecraft landing operation information of a user, comparing the position of the dynamically marked spacecraft on a landing track with the spacecraft landing track information, comparing the spacecraft landing operation information with the spacecraft landing teaching information, and obtaining a comparison result, wherein the spacecraft landing operation information comprises at least one of spacecraft direction operation information, power operation information and spacecraft attitude information;
the state scoring module is used for scoring the simulation operation state of the user according to the comparison result; the state scoring module further comprises: the first scoring submodule is used for judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the information of the landing orbit of the spacecraft, if so, adding a mark adding identifier to the simulated operation state of the user, and otherwise, adding a mark subtracting identifier to the simulated operation state of the user; the second scoring submodule is used for judging whether the spacecraft login operation information is consistent with corresponding information in the spacecraft login teaching information, if so, adding a score adding identifier to the simulated operation state of the user, and otherwise, adding a score subtracting identifier to the simulated operation state of the user;
after judging whether the position of the dynamically marked spacecraft on the landing orbit is consistent with the information of the landing orbit of the spacecraft, the module is further used for: if the position of the dynamically marked spacecraft on the landing orbit is determined to be inconsistent with the information of the landing orbit of the spacecraft, detecting a deviation value between the position of the dynamically marked spacecraft on the landing orbit and the landing orbit; calculating a score reduction value of the simulation operation state of the user according to the deviation value, and taking the score reduction value as the score reduction identification;
after judging whether the spacecraft login operation information is consistent with the corresponding information in the spacecraft login teaching information, the module is further configured to: if the spacecraft landing operation information is determined to be consistent with the corresponding information in the spacecraft landing teaching information, detecting the timeliness of a user for the spacecraft landing operation; calculating a scoring value of the simulation operation state of the user according to the timeliness, and taking the scoring value as the scoring identifier;
a continuous adding and dividing detection module: after adding the bonus mark to the simulated operation state of the user, detecting whether the bonus mark is continuously added to the simulated operation state of the user for multiple times, if so, increasing the bonus mark to the simulated operation state of the user, and taking the increased bonus mark as an additional bonus mark;
the result counting module is used for counting the scoring result of the simulation operation state of the user after the spacecraft is determined to log in the planet to be logged;
the state display module is used for calculating the residual fuel information of the spacecraft according to the navigation time and the navigation mileage of the spacecraft and the preset fuel information of the spacecraft; acquiring the remaining mileage from the earth to a planet to be landed; calculating the remaining navigable time and/or the remaining navigable mileage according to the remaining fuel information and the remaining mileage; and taking the navigation time, the navigation mileage, the residual fuel information, the residual mileage and the residual navigable time and/or the residual navigable mileage as the states of the spacecraft and displaying the states.
6. An electronic device, comprising
A processor; and
a memory having computer readable instructions stored thereon which, when executed by the processor, implement the method of any of claims 1-4.
7. A computer program comprising computer program code to be loaded into a computer system and executed to perform the steps of the method according to any of claims 1-4.
8. A computer readable storage medium having stored thereon a computer program comprising claim 7.
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| PCT/CN2018/092771 WO2019165730A1 (en) | 2018-03-02 | 2018-06-26 | Teaching method and apparatus for simulating planetary landing |
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