CN111710209B - Model rocket demonstration system and demonstration method thereof - Google Patents
Model rocket demonstration system and demonstration method thereof Download PDFInfo
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- CN111710209B CN111710209B CN202010719574.XA CN202010719574A CN111710209B CN 111710209 B CN111710209 B CN 111710209B CN 202010719574 A CN202010719574 A CN 202010719574A CN 111710209 B CN111710209 B CN 111710209B
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- 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
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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
- G09B25/00—Models for purposes not provided for in G09B23/00, e.g. full-sized devices for demonstration purposes
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Abstract
The application discloses model rocket demonstration system and demonstration method thereof relates to teaching aid model technical field, and the demonstration system includes: the teaching terminal equipment is used for sending a control instruction; the model rocket shell is provided with a simulated rocket ground interface and is used for receiving a control instruction; the simulation control components are respectively arranged in the shell or on the surface of the simulation rocket shell, and part of the simulation control components are also connected with the simulation rocket ground interface and used for responding to control instructions; the visible light path is used for connecting part of the analog control components and connecting part of the analog control components with the analog rocket ground interface; each visible light path is respectively connected with the simulated rocket ground interface and used for responding to a control instruction to turn on light emission or turn off the light emission so as to demonstrate the single step debugging, launching and flying process of the rocket. The method and the device can be completely and independently used for training and teaching, simulating the single-step debugging control operation of the rocket, and simulating the relevant actions of the whole rocket launching and flying process.
Description
Technical Field
The application relates to the technical field of teaching aid models, in particular to a model rocket demonstration system and a demonstration method thereof.
Background
Rocket launching and flying processes are very complex, and have irreversibility and irreproducibility. If training and teaching of rocket launching operation are carried out through real equipment, the defects of limited training field, high cost, long period and the like exist. At present, simulation training equipment is gradually used at home and abroad to replace real equipment for training and teaching.
In the related art, the training methods are mainly classified into two types: one is based on a virtual reality technology, a virtual scene is manufactured, and trainees can finish operation training indoors, but the problems of poor immersion feeling, insufficient training effect and the like of the trainees exist; and the other type is to set up a simulation training platform for rocket launching operation, mainly arrange a simulation and aid decision-making system and a demonstration system in a training area to finish related teaching such as rocket transportation, test, erection and launching flow control, wherein the flow after rocket ignition is a simulation image, and the problems of insufficient experience, poor learning effect and the like exist.
Disclosure of Invention
Aiming at one of the defects in the prior art, the application aims to provide a model rocket demonstration system and a demonstration method thereof so as to solve the problems of poor immersion and insufficient training effect of trained personnel in the related technology.
A first aspect of the application provides a model rocket demonstration system comprising:
the teaching terminal equipment is used for sending control instructions, and the control instructions comprise single-step debugging instructions, launching instructions and flight instructions of the rocket;
the model rocket shell is provided with a simulated rocket ground interface, and the simulated rocket ground interface is in communication connection with the terminal equipment and is used for receiving the control command;
a plurality of analog control components, which are respectively arranged in the shell or the surface of the analog rocket shell, and part of the analog control components are also connected with the analog rocket ground interface and used for responding to the control command to execute corresponding actions;
the visible light path is used for connecting part of the simulation control components and connecting part of the simulation control components with the simulation rocket ground interface to form a model rocket of the simulation rocket;
each visible light path is respectively connected with the simulated rocket ground interface and used for responding to the control instruction to turn on light or turn off not to emit light so as to demonstrate the single step debugging, launching and flying process of the rocket.
In some embodiments, the analog control unit includes:
a plurality of analog electronic devices for simulating respective electronic devices of the rocket, the plurality of analog electronic devices including a master electronic device and a plurality of slave electronic devices;
a plurality of simulation executing mechanisms which are respectively used for simulating each executing mechanism of the rocket and responding to the control instruction to execute corresponding actions;
the plurality of simulation initiating explosive devices are respectively used for simulating each initiating explosive device of the rocket and responding to the control instruction to execute corresponding actions;
and a plurality of analog power supply devices for simulating the power supply devices of the rocket, respectively, wherein the analog power supply devices include a first analog power supply and a second analog power supply.
In some embodiments, the model rocket case comprises at least:
the instrument cabin section is positioned at the head, the main electronic equipment and part of slave electronic equipment are arranged in the instrument cabin section, and the first analog power supply is also arranged;
and the power cabin section is positioned at the tail part, and residual slave electronic equipment and the second analog power supply are arranged in the power cabin section.
In some embodiments, the visible light path comprises a power supply visible light path for simulating power supply, a communication visible light path for simulating communication, and an activation visible light path for simulating an activation response;
the power supply visible light path, the communication visible light path and the activation visible light path are light paths formed by lamp belts with different colors respectively.
In some embodiments, the power supply visible light path includes:
the first power supply optical path is used for connecting the simulation rocket ground interface and the main electronic equipment;
a second power supply optical path for connecting the first analog power supply and the main electronic device;
a third power supply optical path for connecting the master electronic device to each of the plurality of slave electronic devices in the equipment room section;
a fourth power supply optical path for connecting the slave electronic device in the power compartment section and the third power supply optical path;
a fifth power supply optical path for connecting the second analog power supply to a plurality of analog actuators, respectively;
and a sixth power supply optical path for connecting the simulated rocket ground interface with a plurality of simulated actuators respectively.
In some embodiments, the visible light communication path includes:
a first communication optical path for connecting the master electronic device to a plurality of slave electronic devices in the instrument bay section, respectively;
a second communication optical path for connecting the slave electronic device in the power compartment section and the first communication optical path;
and the third communication optical path is used for connecting the analog arrow-ground interface and the second communication optical path.
In some embodiments, a plurality of the above activated visible light paths respectively connect each simulated initiating explosive device with its corresponding simulated electronic device.
In some embodiments, the simulated rocket case is made of transparent materials.
In some embodiments, the teaching terminal device is a mobile terminal or a PC, and the teaching terminal device and the arrow-ground interface are in wired or wireless communication connection.
A second aspect of the present application provides a demonstration method of the model rocket demonstration system, which includes the steps of:
the teaching terminal equipment sends a control instruction to the simulated rocket-ground interface;
the simulated rocket ground interface controls part of the simulated control components to execute corresponding actions according to the received control instructions and controls each visible light path to be switched on to emit light or switched off not to emit light so as to demonstrate the single-step debugging, launching and flying processes of the rocket.
The beneficial effect that technical scheme that this application provided brought includes:
the model rocket demonstration system and the demonstration method thereof have the advantages that the teaching terminal equipment is matched with the simulated rocket for use, the control instruction sent by the teaching terminal equipment is received through the simulated rocket-ground interface on the simulated rocket shell, the control part simulates the control part to respond to the control instruction to execute corresponding actions and control each visible light path to be switched on to emit light or not to emit light when being switched off, so that the single-step debugging, launching and flying processes of the rocket are demonstrated, and therefore, the model rocket demonstration system and the demonstration method thereof can be completely and independently used for training and teaching, simulate the debugging control operation of the rocket, and simulate the related actions of the whole process of launching and flying of the rocket, and therefore, trained personnel can be subjected to full, comprehensive and repeated flow decomposition, theoretical knowledge training, fault processing teaching and the like at lower cost, dependence on real equipment is reduced, and comprehensive quality of the trained personnel is rapidly improved.
Drawings
FIG. 1 is a schematic structural diagram of a model rocket provided in an embodiment of the present application;
fig. 2 is a schematic connection diagram of a communication visible light path provided in an embodiment of the present application;
fig. 3 is a schematic connection diagram of a power supply visible light path provided in an embodiment of the present application;
FIG. 4 is a schematic diagram of a connection for activating a visible light path according to an embodiment of the present application;
FIG. 5 is a control schematic diagram of an analog actuator according to an embodiment of the present disclosure;
fig. 6 is a schematic diagram of an exemplary method according to an embodiment of the present disclosure.
Detailed Description
The present application will be described in further detail with reference to the accompanying drawings and examples.
Referring to fig. 1, the embodiment of the present application provides a model rocket demonstration system, which may be applied to training and teaching of a whole rocket launching and flying process in an army, a college, or a scientific research unit. The model rocket demonstration system comprises teaching terminal equipment, a simulation rocket shell, a simulation control part and a visible light path.
The teaching terminal equipment is used for sending control instructions, and the control instructions comprise single-step debugging instructions, launching instructions and flight instructions of the rocket. The single-step debugging instruction comprises instructions of power distribution, power failure, work turning, safety turning, battery activation, power turning, ignition and the like.
The model rocket shell is provided with a simulated rocket ground interface (in fig. 1, the simulated rocket ground interface is separately shown for more clearly showing the connection relationship between the simulated rocket ground interface and part of the simulated control components), the simulated rocket ground interface is in communication connection with the terminal equipment, and the simulated rocket ground interface is used for receiving the control command sent by the teaching terminal equipment.
The simulation control components are arranged in the simulation rocket shell or on the surface of the simulation rocket shell and used for simulating relevant equipment of a real rocket. And the part of the simulation control component is also connected with the simulation rocket ground interface and used for responding to the control command to execute corresponding actions.
The visible light path is used for connecting part of the simulation control components, and is also used for connecting part of the simulation control components with the simulation rocket ground interface to form a model rocket of the simulation rocket.
And each visible light path is respectively connected with the simulated rocket ground interface and used for responding to the control instruction to turn on light or turn off not to emit light so as to demonstrate the single step debugging, launching and flying process of the rocket.
The model rocket demonstration system of the embodiment is characterized in that the teaching terminal equipment is matched with the simulated rocket for use, the control instruction sent by the teaching terminal equipment is received through the simulated rocket-ground interface on the simulated rocket shell, the control part simulates the control part to respond to the control instruction to execute corresponding actions and controls each visible light path to be switched on to emit light or not to emit light when being switched off so as to demonstrate the single-step debugging, launching and flying processes of the rocket, therefore, the model rocket demonstration system can be completely and independently used for training and teaching, simulate the single-step debugging control operation of the rocket and simulate the related actions of the whole rocket launching and flying processes, so that the trained personnel can be subjected to full, comprehensive and repeated flow decomposition, theoretical knowledge training, fault processing teaching and the like at lower cost, the dependence on real equipment is reduced, and the comprehensive quality of the trained personnel is rapidly improved.
In this embodiment, the model rocket can be powered by the external mains supply or by a self-contained rechargeable battery.
Optionally, the analog control component includes analog electronic equipment, an analog actuator, an analog initiating explosive device and an analog power supply equipment.
The plurality of simulation electronic devices are respectively used for simulating each electronic device in the real rocket. The analog electronic device includes a master electronic device and a plurality of slave electronic devices.
In this embodiment, the master electronic device is an rocket-mounted computer simulating the inside of a real rocket, and the plurality of slave electronic devices include electronic devices simulating a cabin controller, a satellite navigation receiver, an inertial device and the like inside the real rocket. In the real rocket, the rocket-mounted computer is respectively communicated with each slave electronic device and sends related commands and information to each slave electronic device, and each slave electronic device responds to the related commands and information to respectively control corresponding initiating explosive devices and actuating mechanisms. In this embodiment, the plurality of slave electronic devices include a first slave electronic device, a second slave electronic device, a third slave electronic device, and a fourth slave electronic device.
The plurality of simulation executing mechanisms are respectively used for simulating each executing mechanism of a real rocket and responding to the control instruction to execute corresponding actions, such as simulating pendulum spraying, simulating pendulum rudder pieces and other related actions. In this embodiment, the plurality of simulation actuators includes a first simulation actuator, a second simulation actuator, and a third simulation actuator.
The plurality of simulation initiating explosive devices are respectively used for simulating each initiating explosive device of the real rocket and responding to the control instruction to execute corresponding actions. The simulation initiating explosive device mainly simulates the detonation operation of the initiating explosive device in the rocket in the flight process by playing explosion sound or releasing smoke and the like.
The plurality of simulation power supply devices are respectively used for simulating each power supply device of the real rocket and mainly simulate to supply power to each simulation electronic device, each simulation execution mechanism and the like. The analog power supply device includes a first analog power supply and a second analog power supply.
Optionally, the model rocket case comprises at least an instrument cabin section at the head and a power cabin section at the tail. The instrument cabin section is internally provided with the main electronic equipment, partial slave electronic equipment and the first analog power supply, and the power cabin section is internally provided with the residual slave electronic equipment and the second analog power supply.
In this embodiment, the instrument bay section includes a first bay section and a second bay section, and the power bay section includes a third bay section and a fourth bay section. The master electronic device, the first slave electronic device and the second slave electronic device are all arranged in the first cabin section, the third slave electronic device is arranged in the second cabin section, and the fourth slave electronic device is arranged in the fourth cabin section. The first simulation executing mechanism, the second simulation executing mechanism and the third simulation executing mechanism are all arranged on the fourth cabin section. A first analog power supply is disposed within the first bay and a second analog power supply is disposed within the fourth bay.
Further, the visible light path includes a power supply visible light path for analog power supply, a communication visible light path for analog communication, and an activation visible light path for analog activation response.
The power supply visible light path, the communication visible light path and the activation visible light path are light paths formed by lamp belts with different colors respectively. Optionally, the power supply visible light path is a red light band, the communication visible light path is a blue light band, and the activation visible light path is a yellow light band, so that a power supply path, a communication path and an initiating explosive device activation path when the real rocket works can be simulated. Optionally, each visible light path may further be distinguished by a horse race light strip of a different color.
In this embodiment, the power supply visible light path includes a first power supply light path, a second power supply light path, a third power supply light path, a fourth power supply light path, a fifth power supply light path, and a sixth power supply light path.
The first power supply optical path is used for connecting the simulation rocket ground interface and the main electronic equipment; the second power supply optical path is used for connecting the first analog power supply with the main electronic equipment; the third power supply optical path is used for connecting the main electronic equipment with a plurality of slave electronic equipment in the instrument cabin section respectively; the fourth power supply optical path is used for connecting fourth slave electronic equipment in the power cabin section with the third power supply optical path; the fifth power supply optical path is used for connecting the second analog power supply with a plurality of analog execution mechanisms respectively; and the sixth power supply optical path is used for connecting the simulated rocket ground interface with a plurality of simulated actuating mechanisms respectively.
In this embodiment, the communication visible light path includes a first communication light path, a second communication light path, and a third communication light path.
The first communication optical path is used for connecting the main electronic equipment with a plurality of slave electronic equipment in the instrument cabin section respectively; the second communication optical path is used for connecting fourth slave electronic equipment in the power cabin section with the first communication optical path; and the third communication light path is used for connecting the analog arrow-ground interface and the second communication light path.
In this embodiment, the plurality of activated visible light paths respectively connect each simulated initiating explosive device with its corresponding simulated electronic device.
Preferably, the simulated rocket shell is made of transparent materials, so that trainees can visually and intuitively observe the relevant simulated phenomena.
In this embodiment, after the simulated rocket-ground interface receives the control instruction sent by the teaching terminal device, a training or teaching mode is selected first, then the flashing or extinguishing of a specific visible light path inside the model rocket is controlled according to a program, and when the operation of initiating explosive devices is simulated and activated in the rocket flight flow, a speaker on the simulated initiating explosive devices is controlled to play the explosive sound of the initiating explosive devices, and the motor action of a simulated execution mechanism inside the model rocket is controlled, so as to drive the actions of a simulated rudder piece and a swinging jet. Through the process, corresponding training or teaching demonstration can be completed.
Referring to fig. 2, optionally, the process of simulating communication between electronic devices inside a real rocket specifically includes:
before the simulated real rocket is ignited, the simulated rocket-ground interface on the model rocket controls all communication visible light paths to be bright to form visible light paths; after the simulated real rocket is ignited and before the head body is separated, the simulated rocket-ground interface controls the first communication light path and the second communication light path to be continuously on, and controls the third communication light path to be off; after the simulated real rocket head body is separated, the simulated rocket-ground interface controls the communication circuit lamp strip 1 to be continuously bright and controls the second communication light path to be extinguished.
Referring to fig. 3, optionally, the process of simulating the internal power supply path of the real rocket specifically includes:
before the simulated real rocket is ignited, because the real rocket is powered by the ground, the simulated rocket ground interface on the model rocket controls the first power supply light path, the third power supply light path, the fourth power supply light path and the sixth power supply light path to be all bright to form a visible light path, and controls the second power supply light path and the fifth power supply light path to be not bright to form an open circuit; after the simulated real rocket is ignited and before the head body is separated, the simulated rocket ground interface controls the second power supply light path, the third power supply light path, the fourth power supply light path and the fifth power supply light path to be all on, and controls the first power supply light path and the sixth power supply light path to be off; after the simulated real rocket body is separated, the simulated rocket ground interface controls the second power supply light path and the third power supply light path to be continuously bright and controls the fourth power supply light path and the fifth power supply light path to be extinguished.
Referring to fig. 4, optionally, the process of simulating the activation of a certain initiating explosive device in the real rocket specifically includes:
the simulation rocket ground interface controls the corresponding activation visible light path to be bright and controls the corresponding loudspeaker or loudspeaker on the simulation initiating explosive device to emit detonation sound.
In this embodiment, the plurality of simulated explosive devices include a first simulated explosive device located in the first cabin section, a second simulated explosive device located in the third cabin end, and a third simulated explosive device and a fourth simulated explosive device located in the fourth cabin section. The main electronic equipment is connected with the first simulation initiating explosive device through a first activation light path, the second slave electronic equipment is connected with the second simulation initiating explosive device through a second activation light path, the fourth slave electronic equipment is connected with the third simulation initiating explosive device through a third activation light path, and the fourth slave electronic equipment is connected with the fourth simulation initiating explosive device through a fourth activation light path.
In this embodiment, when the second simulated initiating explosive device is a head-body separation initiating explosive device, a separation popping-up device may be further added between the second cabin section and the third cabin section, and after the second activated visible light path is lit up, the second cabin section and the third cabin section are separated, so that the head body of the simulated rocket is separated.
Referring to fig. 5, optionally, the process of simulating the action of the actuator in the flight process of the real rocket specifically includes:
after receiving the control instruction of the teaching terminal equipment, the simulation arrow-ground interface sends out a motor control instruction according to the preset instruction, so that the corresponding simulation execution mechanism acts at the corresponding moment in the process.
Specifically, when the simulated rocket-ground interface sends a first control command to the first simulated execution mechanism, the first simulated execution mechanism carries out response action; when the simulated rocket-ground interface sends a second control command to the second simulated execution mechanism, the second simulated execution mechanism carries out response action; and when the simulated rocket-ground interface sends a third control command to the third simulated execution mechanism, the third simulated execution mechanism carries out response action.
Optionally, the teaching terminal device is a mobile terminal or a PC terminal, and the teaching terminal device is in wired or wireless communication connection with the rocket-ground interface. Through the communication between the teaching terminal equipment and the simulation rocket-ground interface, the teaching terminal equipment is utilized to realize the training and teaching operations related to the whole process from ground power distribution, work transfer, battery activation, power transfer and the like to ignition, to launching and flying.
Preferably, the model rocket of the embodiment can be matched with a rocket launching operation simulation training platform for use, relevant actions of the rocket in the processes of transporting, testing, erecting, launching process control and the like of the rocket are simulated, non-training time in training is greatly reduced, psychological quality and cooperation capacity of trained personnel are improved, and optimization of rocket launching and flight processes can be promoted.
Optionally, the model rocket and the rocket launching operation simulation training platform are electrically interconnected in a wired or wireless mode. Launching, flight procedure related training and teaching operations can be completed by a computer inside the rocket launching operation simulation training platform.
Referring to fig. 6, an embodiment of the present application further provides a demonstration method of a model rocket demonstration system, which includes the steps of:
s1, the teaching terminal equipment sends a control instruction to the simulated rocket-ground interface.
And S2, the simulated rocket-ground interface controls part of the simulated control components to execute corresponding actions according to the received control instructions, and controls each visible light path to be switched on to emit light or not to emit light when being switched off so as to demonstrate the single-step debugging, launching and flying processes of the rocket. The single-step debugging instruction comprises instructions of power distribution, power failure, work turning, safety turning, battery activation, power turning, ignition and the like, and is used for simulating and demonstrating execution display on a real rocket corresponding to the single switching value instruction.
In this embodiment, the model rocket and the internal simulation electronic device, the simulation executing mechanism, the simulation power supply device and the simulation initiating explosive device thereof are scaling models of a real rocket and relevant devices and components inside the rocket, have a demonstration function, and can cooperate with the launching and flight processes of the model rocket to display relevant signals and execute relevant actions.
Through the model rocket, training and teaching operation demonstration of a single step debugging mode, a simulated real flight mode, a simulated fault flight mode and the like can be completed. The lighting of the power supply visible light path and the communication visible light path represents that communication flow and a power supply loop between corresponding electronic equipment are simulated in the flight process; and activating the lighting of the visible light path, and simulating the activation and detonation of the related initiating explosive device in a specific node of the flight flow after the corresponding simulated initiating explosive device sends out the audio-visual effect.
The demonstration method is suitable for the demonstration systems, can simulate the working process of a real rocket, is safe and reliable, has strong practicability, and can efficiently improve the comprehensive quality of trained personnel.
The present application is not limited to the above embodiments, and it will be apparent to those skilled in the art that various modifications and improvements can be made without departing from the principle of the present application, and such modifications and improvements are also considered to be within the scope of the present application. Those not described in detail in this specification are within the skill of the art.
Claims (8)
1. A model rocket demonstration system, comprising:
the teaching terminal equipment is used for sending control instructions, and the control instructions comprise single-step debugging instructions, launching instructions and flight instructions of the rocket;
the model rocket shell is provided with a simulated rocket ground interface, and the simulated rocket ground interface is in communication connection with the terminal equipment and is used for receiving the control command;
the simulation control components are respectively arranged in the shell or the surface of the simulation rocket shell, and part of the simulation control components are also connected with the simulation rocket ground interface and used for responding to the control command to execute corresponding actions;
the visible light path is used for connecting part of the simulation control components and connecting part of the simulation control components with the simulation rocket ground interface to form a model rocket of the simulation rocket;
each visible light path is respectively connected with the simulated rocket ground interface and used for responding to the control instruction to turn on light emission or turn off and not emit light so as to demonstrate the single step debugging, launching and flying processes of the rocket;
the analog control part includes:
a plurality of analog electronic devices for respectively simulating each electronic device of the rocket, the plurality of analog electronic devices including a master electronic device and a plurality of slave electronic devices;
the simulation execution mechanisms are respectively used for simulating each execution mechanism of the rocket and responding to the control instruction to execute corresponding actions;
the plurality of simulation initiating explosive devices are respectively used for simulating each initiating explosive device of the rocket and responding to the control instruction to execute corresponding actions;
the power supply equipment comprises a plurality of analog power supply equipment, a plurality of analog power supply equipment and a plurality of control equipment, wherein the analog power supply equipment is respectively used for simulating each power supply equipment of the rocket and comprises a first analog power supply and a second analog power supply;
the visible light path comprises a power supply visible light path for simulating power supply, a communication visible light path for simulating communication and an activation visible light path for simulating activation response;
the power supply visible light path, the communication visible light path and the activation visible light path are light paths formed by lamp belts with different colors respectively.
2. A model rocket demonstration system according to claim 1 wherein said model rocket case comprises at least:
the instrument cabin section is positioned at the head, the main electronic equipment and part of the auxiliary electronic equipment are arranged in the instrument cabin section, and the first analog power supply is also arranged in the instrument cabin section;
and the power cabin section is positioned at the tail part, and residual slave electronic equipment and the second analog power supply are arranged in the power cabin section.
3. A model rocket presentation system as claimed in claim 2 wherein said electrically powered visible light path comprises:
the first power supply optical path is used for connecting the simulated rocket ground interface and the main electronic equipment;
a second power supply circuit for connecting a first analog power supply to the main electronic device;
a third power supply optical path for connecting the master electronic device with a plurality of slave electronic devices within the instrument bay section, respectively;
a fourth power supply optical path for connecting the slave electronic equipment in the power compartment section with the third power supply optical path;
a fifth power supply optical path, configured to connect the second analog power supply to a plurality of analog actuators, respectively;
and the sixth power supply optical path is used for connecting the simulated rocket ground interface with a plurality of simulated actuating mechanisms respectively.
4. A model rocket presentation system as claimed in claim 2 wherein said communication visible light path comprises:
a first communication optical path for connecting the master electronic device with a plurality of slave electronic devices in the instrument bay section, respectively;
the second communication light path is used for connecting the slave electronic equipment in the power cabin section with the first communication light path;
and the third communication light path is used for connecting the simulated rocket ground interface and the second communication light path.
5. A model rocket demonstration system according to claim 2 wherein: and the plurality of activated visible light paths respectively connect each simulated initiating explosive device with the corresponding simulated electronic equipment.
6. A model rocket demonstration system according to claim 1 wherein: the simulated rocket shell is made of transparent materials.
7. A model rocket demonstration system according to claim 1 wherein: the teaching terminal equipment is a mobile terminal or a PC end, and the teaching terminal equipment is in wired or wireless communication connection with the rocket ground interface.
8. A method of demonstrating a model rocket demonstration system according to any one of claims 1 to 7, comprising the steps of:
the teaching terminal equipment sends a control instruction to the simulated rocket-ground interface;
the simulated rocket ground interface controls part of the simulated control components to execute corresponding actions according to the received control instructions, and controls each visible light path to be switched on to emit light or switched off not to emit light so as to demonstrate the single-step debugging, launching and flying processes of the rocket.
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| KR100330983B1 (en) * | 2000-02-03 | 2002-04-01 | 윤여형 | Water rocket a launching pad |
| CN102819976A (en) * | 2012-09-10 | 2012-12-12 | 施胜南 | Water injection and air inflation integrated water rocket launching device |
| CN204215628U (en) * | 2014-04-23 | 2015-03-18 | 郭勤怡 | A kind of model rocket teaching aid |
| CN106297524A (en) * | 2016-04-23 | 2017-01-04 | 江苏华明科教设备有限公司 | A kind of rocket launching analog device and method of work thereof |
| CN206601830U (en) * | 2017-03-01 | 2017-10-31 | 蓝色智库（北京）科技发展有限公司 | Submarine based on simulation model integrates experience display systems |
| CN107154204B (en) * | 2017-07-06 | 2023-09-05 | 中国科学技术馆 | Rocket launching demonstration device and demonstration method |
| CN207233259U (en) * | 2017-07-06 | 2018-04-13 | 中国科学技术馆 | Rocket launching apparatus for demonstrating |
| CN208325305U (en) * | 2018-06-08 | 2019-01-04 | 朱梓熙 | Cart is used in model rocket transmitting |
| CN110718131A (en) * | 2019-10-14 | 2020-01-21 | 唐山维数科技有限公司 | Launching device for simulating rocket launching |
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