The system of observation and monitoring polarice

Abstract

The invention of system of observation and monitoring the earth warming and changes in polar ice behavior using LoRa to satellite technology is a system for measuring, observing and monitoring weather and environmental conditions in order to determine the effects of environmental conditions and climate changes on the way ice masses change in the polar regions of the earth. This invention is related to the rocket equipped with several modules for measuring the conditions of the surrounding environment as well as data transmission through the LoraWan protocol to a fixed or deployable station. Also, in this invention, if there is a need to calibrate any of the modules in the meteorological rocket, the central server structure, which is equipped with an artificial intelligence analyzer, can calibrate the device by comparing the arrays received from the surrounding rockets and analyzing the data received from these systems.

Description

[0001] TITLE OF INVENTION

[0002] THE SYSTEM OF OBSERVATION AND MONITORING POLARICE

[0003] TECHNICAL FIELD OF THE INVENTION

[0004] The present invention is related to the system for measuring, observing and monitoring weather and environmental conditions in order to determine the effects of climate change on the manner of changing the polar ice masses, as well as the effect of changes in the amount of atmospheric pollutants and greenhouse gases on the ice mass and also related to the rocket equipped with several modules for measuring the conditions of the surrounding environment and also related to data transmission through the LoraWan protocol to a fixed or deployable station.

[0005] PRIOR ARTS

[0006] Global warming begins with a phenomenon known as the greenhouse effect. There is a balance between the earth's atmosphere and the beams received from the sun. The quick climate changes we are observing now are mostly due to human use of oil, gas and coal for homes, factories and transportation. When these fossil fuels burn, they release greenhouse gases, which trap the sun's heat and cause the planet's temperature to rise. The known greenhouse gases include water vapor, carbon dioxide (CO2), methane (CH4) and nitrogen oxide (N2O), which the most common is carbon dioxide. Some of the CO2 in the atmosphere is due to natural activities. According to the research of scientists, the temperature of the earth has increased by 1.2 degrees of centigrade compared to the 19th century (before industrialization), and this amount will reach 1.5 degrees of centigrade in the mid- 2030s. Also, the amount of CO2 in the atmosphere has increased by 50%. Although, the 1.5 degrees of centigrade increase in temperature in the last 150 years does not seem so dangerous. But the evidence shows the opposite, because every 0.5°C increase in the earth's heat has a great impact on the increase of heat waves and the severity of agricultural and environmental droughts.

[0007] The frozen part is connected with other parts of the earth system. What happens in the cryosphere affects the entire earth. It has been heard that climate change will increase the temperature and the polar ice caps will melt. Most of these ices are located in the North and South Poles, the whole planet will be affected by the melting of these ices. Therefore, what happens in the cryosphere does not remain only in the cryosphere.

[0008] Some of the reasons changes in the cryosphere affect the entire planet are feedbacks that cause more warming. Currently, scientists are studying how the frozen poles on Earth affect the rate of climate change. In the following, we discuss some effects of the melting of the cryosphere on climate change through interaction with other parts of the system and feedbacks that increase the rate of global warming.

[0009] When sunlight hits ice and snow, more than 90 percent of it is reflected back into space, since global warming causes more snow and ice to melt in the summer, the ocean and land beneath the ice on the earth's surface came out from under its ice shield, and since they are darker in color, these parts absorb more solar radiation and then transfer this heat to the atmosphere. This will cause more earth warming. So the ice melting cause more warming and more ice melting as the result. This is the most important feedback of global warming. According to a recent scientific study that used computer models to predict the future of Arctic ice, it is predicted that there will be no more icebergs left in the Arctic Ocean during the summer in the next few decades. Therefore, by monitoring the melting of the polar ice caps, the amount of global warming can be checked.

[0010] In the same area, NASA is preparing to launch a modern, laser-equipped satellite that will monitor, investigate and study the changes in the Earth's glaciers for three years. This mission called "ICESat-2" will start in mid-September. This satellite will be able to measure the changing thickness of the earth's glaciers from season to season and record their increase and decrease in thickness with an accuracy of half a centimeter. It is worth noting that the investigated areas are very vast and the size of the American continent or larger, and the changes that occur on them are very small. This satellite is the size of a car and is able to take continuous measurements in a very precise way over a large area. But building and sending a satellite into space is a very expensive and time-consuming method.

[0011] In the field of technology to investigate the melting of polar ice, many studies have been conducted and patents have been registered, some of which are described below, including an Chinese invention with patent number CN107933832A which is granted dated 16 / 04 / 2019 titled " Polar ice base sea ice monitoring buoy and polar ice base sea ice parameter monitoring method" discloses a kind of polar ice base sea ice monitoring buoy and a kind of polar ice base sea ice parameter monitoring method, there are the protecting bin and aircraft, controller storehouse, battery compartment and the telescope support of standard type bottom for placing aircraft in buoy standard type. In measuring method, various kinds of sensors is carried using aircraft, the atmospheric parameter of more than ice face different height in 10 meters can be measured, wind speed and direction, air temperature and air pressure including different height, the sonar to measure waterborne distance at face snowfall altitude information and underwater sonar measurement subglacial interface on ice, can obtain the change of ice sheet gross thickness. The GPS position information carried by reading in iridium satellite module obtains the position signal of buoy, data pass through iridium satellite module transfer, realize that automation remote monitors in real time, analysis foundation is provided for the thermodynamics change procedure in sea ice growth course, can be applied to the unmanned monitoring of automation of south poles polar region sea ice.

[0012] In another Chinese invention with patent number CN10445771 IB which is granted dated 23 / 06 / 2017 titled "Arctic Ocean shallow water type pull-type thermohaline depth monitoring system" relates to a kind of Arctic Ocean shallow water type pull- type thermohaline depth monitoring system. Including: For meteorological observation and control, satellite communication, the ice base buoyage of power supply, for buoyancy conversion and elevating control, carry out ocean temperature, salinity, the underwater section sounding buoy device of depth survey and the connection for ice base buoyage and underwater section sounding buoy device, there is provided data signal line, high strength tension cable, the high intensity trailing cable device of the vulcanized joint of seawater corrosion resistance. The present invention can carry out thermohaline depth profile survey under water, fathom as 0 120 meters under ice sheet, filled up 120 meters of off- lying sea in the world and, with the deficient blank of shallow observation method, realized the same area hydrology and meteorological simultaneous observation, The lithium battery power supply system of the use vast capacity of the system, improves the service life of system, and the invention has very big application value, can promote the use of the association area for being engaged in polar region research in the world.

[0013] In an international invention with publication number W02009029129A1 which is filed dated 17 / 05 / 2008 titled "Air-deployable expendable ice buoy" in WIPO is an Air-Deployable Expendable Ice Buoy (AXIB) that can withstand multiple freeze - thaw cycles and operate equally well in ice prone ocean or fresh water. The AXIB can be dropped from an airborne platform, land on an ice surface, right itself to the vertical position, anchor and stabilize itself in the ice, withstand several freeze - thaw cycles and continue to transmit data while anchored to the ice or floating in the ocean. The AXIB is designed so that it can be dropped onto marginal ice via parachute from a plane or helicopter. When the buoy reaches the surface of the ice, an explosive cutter severs a cinching cable at the base of the deployment cone. This separates the two halves of the cone, and allows the cone halves and parachute to fall away. Upon reaching the surface, the AXIB will invariably be in other than upright position. The erection legs will then actuate and raise the AXIB to the full upright position. Once in the upright position, the ice anchor is actuated. The ice anchor utilizes an exothermic chemical reaction contained within a hollow pipe that penetrates by melting into the ice. An alternative method of anchoring can be achieved by mechanical drill, screw and / or percussive methods.

[0014] Also in a Chinese invention with patent number CN2689229Y which is granted dated 30 / 03 / 2005 titled "Automatic monitoring floater of polar region marine environment" relates to an automatic monitoring floater of polar region marine environment, a system integrated equipment which measures marine parameters on condition of the polar region marine environment, comprising the tower of a floater body, an instrument cabin, a buoyancy block, a transducer and a mooring system. The automatic monitoring floater of the polar region marine environment can be overlaid on the ice surface, and can also float on the water surface; the environment parameters is measured through the transducer carried by the floater, and is emitted to a polar rail satellite through the antenna on the tower of the floater body. The measured data is received through utilizing the internet to complete the field measurement and the quasi-real time data transmission of the polar region marine environment. Important polar region meteorology, hydrograph, ice temperature data and the changing rule thereof are provided for the researching of globe marine and climatic environment.

[0015] In another Chinese invention with patent number CN 103481786B which is granted dated 06 / 04 / 2014 titled "A kind of polar region robot based on wind-solar hybrid energy" discloses a kind of polar region robot based on wind-solar hybrid energy, installs the active deformation hitch with wheel in the bilateral symmetry of vehicle body; Two active deformation hitches respectively adopt seven bar Structure composing; By being connected from dynamic deformation hitch between two active deformation hitches; Thus, the height that can realize vehicle body regulates, and body side is to rolling. Vehicle body is also provided with loading device, power equipment supply and control system. Loading device is used for Real-time Obtaining external environment information and polar region robot displacement status information. Power equipment supply comprises aero generator, solar panel and battery pack; The electric energy that aero generator and solar panel export is stored by battery pack. Described control system be used for realizing the control of power equipment supply and polar region robot movement, keep away barrier, obstacle detouring controls. Advantage of the present invention is: can adaptation to the ground better, possesses better complex-terrain carrying capacity, can perform scientific investigation task for a long time at polar region environment. Also, in a Chinese invention with publication number CN108718210A which is filed dated 27 / 06 / 2018 titled "A kind of arctic ice sheet communication platform" discloses a kind of arctic ice sheet communication platforms, including pass sequentially through buoyant structure, communication module and the equipment compartment of fixed link connection, the buoyant structure is configured as being arranged on ice sheet, the communication module is configured as being arranged in ice sheet, the communication positioning antenna in the communication storehouse is located at across the buoyant structure above the ice sheet, the buoyant structure is provided with mounting bracket on one side far from ice sheet, the mounting bracket is vacantly arranged towards the end on the outside of the buoyant structure more than the buoyant structure, one end of the fixed link is fixedly connected with the mounting bracket, the equipment compartment is configured as being arranged under ice sheet, and the equipment compartment is electrically connected with the communication module by cable. One of the present invention has technical effect that the present invention is laid simply, easy for installation, disclosure satisfy that and assembles and lay when ice face is laid.

[0016] And in a Korean invention with patent number KR101082804B1 which is granted dated 11 / 11 / 2011 titled "Sensor coordinator apparatus" provides sensor coordinator apparatus. This invention includes the sensor communication unit for receiving the sensing data sensed by each sensor from one or more sensors; A micro controller unit (MCU) for generating monitoring information from the sensing data through a predetermined algorithm; A memory in which the sensing data and the monitoring information are stored; And a server communication unit which reads out the monitoring information stored in the memory and transmits the monitoring information to the monitoring server every selected period. The sensor coordinator device can monitor the information on the data sensed by the sensor more accurately and quickly while minimizing the load of the server regardless of the installation location or the number of installation of the sensor.

[0017] In an US invention with patent number US8912892B2 which is granted dated 16 / 12 / 2014 titled "Autonomous and controllable systems of sensors and methods of using such systems" an autonomous and controllable system of sensors and methods for using such a system of sensors are described in which The sensor system comprises a plurality of unit sensors, each unit sensor comprising: an inner enclosure; an outer enclosure enclosing the inner enclosure, the outer enclosure including at least one sensing device and a controlling device; and a first elastic layer between an outer surface of the inner enclosure and an inner surface of the outer enclosure, wherein each unit sensor is configured to communicate with other unit sensors within the sensor system; and the plurality of unit sensors in the sensor system form a network of sensors. Moreover, the spherical mobile sensor (100) can exploit temperature differences available when deployed in the regions, for example, large deserts, Polar Regions or open seas, in order to harvest energy using thermopile.

[0018] Also, in another US invention with patent number US9563203B2 which is granted dated 07 / 02 / 2017 titled "Controllable buoys and networked buoy systems" buoyant sensor networks are provided, comprising floating buoys with sensors and energy harvesting capabilities. The buoys can control their buoyancy and motion, and can organize communication in a distributed fashion. Some buoys may have tethered underwater vehicles with a smart spooling system that allows the vehicles to dive deep underwater while remaining in communication and connection with the buoys. The systems of the present disclosure can apply to applications such oil and gas explorations, drilling, as well as transferring oil and gas from the drilling sites to the destination using pipelines or various vessels in the open seas, as well as in the Polar Regions such as the Arctic.

[0019] In another US invention with patent number US4924698A which is granted dated 15 / 05 / 1990 titled "Method and apparatus for remote monitoring of oceanographic conditions" is an apparatus for measuring profiles of ocean properties. The apparatus includes a stationary surface buoy to which a weight and cable are attached, the sensors traverse the cable by means of a hydrofoil the pitch of which is varied by a pressure activated sensing system. The apparatus is adapted for use under pack ice or ice bergs. The method is that of moving the sensors in a vertical direction along a guide cable beneath a surface buoy. The cable can hang from the pack ice or be buoyed upward from an anchor on the sea floor.

[0020] Also in a Japanese invention with patent number JP7146438B2 which is granted dated 04 / 10 / 2022 titled "Light Detection and Ranging (LIDAR) Ice Detection System" is an ice detector including one or more LIDAR devices on an aircraft, each LIDAR device including a transmitter and a receiver, each transmitter being a laser. The pulse is used to repeatedly scan an aerodynamic surface of the aircraft to form a diffuse laser pulse that is diffused from the aerodynamic surface, each of the receivers receiving the diffuse laser pulse and timing the diffuse laser pulse received at the receiver. An ice detector is described that outputs data containing: From the output data, changes in aerodynamic surface coordinates over time indicative of ice accumulation and / or shedding on the aerodynamic surface are calculated.

[0021] Also in an Article written by American researchers and supported by NASA titled "An Intelligent Wind-Opportunistic Mobile Sensor to Monitor the Polar Region" provides sensors capable of operating in harsh environments for long periods of time and having wireless readout capability are needed for mapping environmental conditions in remote areas, such as polar regions. In this paper, we report the first measured results of an innovative in-situ system of controllable and wind- opportunistic spherical mobile sensors (called Moballs), used to monitor and map various environmental factors in polar areas. To have self-powered controlled motion, Moballs exploit the abundance of wind and a novel dual-functioning mechanical control and linear induction system. Moballs have peer-to-peer and Moball-to-base (e.g. satellite) communication capability, reporting the sensory data back to the base station or other peer Moballs for task sharing decisions, improving area coverage, optimizing system performance, etc.

[0022] DESCRIPTION OF THE INVENTION

[0023] The present invention is a system for measuring, observing and monitoring weather and environmental conditions in order to determine the effects of environmental conditions and climate changes on the way ice masses change in the polar regions of the earth, and also the comparison of specific time periods and the effect of changes in the amount of atmospheric pollutants and greenhouse gases on the ice mass. This invention includes a projectile equipped with wings and an speed control system umbrella, the said rocket is made of a steel cylinder made of 316L steel by rolling method and sub-powder welding or argon welding, or made of 316L steel tube with low thickness.

[0024] Figure No. 1 (part one): In the front part of the mentioned capsule, an incomplete cone is formed, which is connected from the base part to the lower part of the cylinder of the capsule by welding method. This incomplete cone is concentric with the cylinder of the capsule and forms the base of the cone at the point of connection with the cylinder of a circular plate. From the upper part of the cone, a steel rod made of anticorrosive mild steel (low-carbon) with welding capability comes out, so that the end part of the rod is welded on the plate separating the incomplete cone from the cylinder. The presence of a central hole in the center of the separation plate makes it possible for the ice temperature probe to be placed in the central part of the rod. Also, the three holes on the vertices of an equilateral triangle provide the possibility of screwing three rods of the entire thread, which are designed to hold the internal devices of the electronic mechanism. Due to the large diameter of the separating plate of the cylinder and the incomplete cone, it is possible to tap the mentioned holes and create suitable conditions for screwing the mentioned rods inside the separating plate.

[0025] The middle of the separating plate up to the tip of the incomplete cone is filled with molten lead in such a way that the lead fills the entire inner space of the cone and serves as a support base for the rocket head rod on the one hand and used as a balancer for the rocket weight distribution on the other hand. In the section close to the base of the rod, the presence of parallel raised plates on the rod makes it possible for the molten lead to surround the base of the rod in such a way that it is not possible to separate the lead from the rod. At the tip of the rod, there is a 60 degree cone with three prominent incomplete cones on the tip of the rod, giving the said rod an arrow shape so that when the rocket hits the ice surface, the rocket can sink into the ice and stabilize the structure of the rocket on the ice. In the inner part of the cylinder, the presence of three fully threaded steel wires makes it possible to place plates made of polycarbonate polymer with a circular shape and similar concentric holes on these three threaded wires in certain places should be strengthened on the triple rods with a bolts and nut from below and another nut from the other plates. PCB plates or printed circuit board used for internal equipment boards are also in the form of circular plates and generally have a certain thickness, which is placed on polymer plates as a shock absorber support and connections are connected to each other. In the used circuits, only dip parts were used in order to not cause a loss in the performance of the soldering joints due to the impact of thermal and cold hits. The rechargeable lithium batteries section is located on the first floor of the structure, and in order, the ice temperature detection module, then the surrounding air temperature detection module, and then the lithium battery charger module with the help of solar cells, and then the LoRaWAN module for sending and receiving information as well as GPS module is mounted in to extract location and height information. The body of the system is connected to the antenna of the structure and the LoRaWAN protocol and plays the role of the antenna for this system, and in the end part, the presence of a plate similar to the plate separating the conical part from the cylindrical part provides the possibility of fixing all three rods of the entire thread. The presence of a narrow ring around the upper part of the cylinder makes it possible for the upper circular plate to be pulled inside the cylinder by tightening its retaining nuts and placed on the step created by the peripheral ring, on the one hand, the heads of all three rods are locked in the separating plate of the bottom of the cylinder, and on the other hand, due to the force coming from the nuts of the upper part of the device plate, strongly pressured the peripheral ring of the lower part and makes possible to fix the floors along with various elements in the mentioned device. The existence of three wings in the lower part allows the correct movement of the rocket in the air. The existence of a small fabric umbrella in the lower part caused the mentioned equipment reaches a certain speed while moving in the air, which this terminal velocity is inversely proportional to the cross-sectional area of the said umbrella. The size of the umbrella is adjusted in such a way that the terminal velocity of the said rocket is adjusted in such a way that the inertia of the motion of the rocket of the present invention can sink its rod into the ice and settle on the ice surface when it hits the ice surface. The mentioned rocket is left at its location by a flying device such as a plane, helicopter or balloon and based on the terminal velocity, the device sinks into the ice. If the number of rockets needed on an ice mass is large, the mentioned device is placed inside a smart magazine equipped with a precise rocket launch system, which consists of two thick rubber belts with an angle equal to the angle of the cone of the rocket head. The discussed rockets are placed on the mentioned conveyor belt and based on the flier coordinates, the height of the device flier from the ice surface and also the topographical map of the ice area, it is moved and released by an artificial intelligence in such a way that with the precise calculation of the desired rules in the discussion of projectiles, collides a specific point. At the time of launching each of the rockets, the ring connected to the speed regulating umbrella is outside the end of the rocket, and when the rocket is thrown due to the weight of the rocket, the device moves towards the ground and the speed regulating umbrella comes out from inside the rocket and adjusts the free fall speed of the rocket towards the ground. When the rocket reaches the ground and collides with the ice masses immediately after the first impact, the internal mechanism of the rocket, which is equipped with a gravity-activated key system, starts the process of activating the internal equipment. The entire interior of the rocket has been filled and coated with a flexible composite resin in such a way that when the rocket collides with ice surfaces, it can prevent the transfer of blows to sensitive parts and also the bending and strains of printed circuit boards and fibers have been minimized and any deformation, bending or breakage has been completely eliminated. The outer part of the rocket from the beginning of the top of the middle cone to the halves of the main cylinder of the body is covered with a cover of dense polyurethane foam. In this part, the polyurethane is reduced by half and a ring-shaped solar cell is placed in the reduced part of the polyurethane diameter. In the upper part of the mentioned ring, the continuation of the Polyurethane cover has returned to the previous diameter and blocks the movement of the mentioned ring. The rocket guiding wings have been removed from the polyurethane cover.

[0026] After launching the rocket from the flying vehicle and colliding one or all of the rockets at the predefined points collected its data from each of the ice temperature measurement module, ambient temperature, air pressure, light intensity (which is a function of receiving light with the help of the solar cell), latitude and longitude coordinates and the height of the device from the surface of the open sea and in competition, previously understandable data packets are transferred by the LoRaWAN module to a fixed or deployable station with the help of aerial vehicles. In the following, the mentioned station transmits its information with the help of telecommunication systems, including sending and receiving information on the Internet or the system of sending and receiving information with the help of satellites. Signals are sent by LoRa protocol and commands are also sent from the central station to the satellite or any other transmission and reception structure. If you need to calibrate any of the modules in the aforementioned meteorological rocket, the structure of the central server, which is equipped with an artificial intelligence analyzer, can calibrate the device by comparing the arrays received from the mentioned nearby rockets and analyzing the information received from these systems and by sending information through LoRaWAN, apply the required commands for the calibration of the equipment as well as the required changes. BRIEF DESCRIPTION OF THE FIGURES

[0027] Figure 1 shows the general and external view of the rocket, which has the following parts:

[0028] 1. Cylindrical body 2. Incomplete cone

[0029] 3. Leading wing

[0030] 4. Central hole

[0031] 5. Fabric umbrella

[0032] 6. Rod base Figure 2 shows the internal view of the rocket, which includes the following parts:

[0033] 2. Incomplete cone

[0034] 6. LoRA board

[0035] 7. Rod

[0036] 8. Spring 9. Thermometer

[0037] 10. Battery

[0038] 11. Measurement modules

[0039] 12. GPS range

[0040] 13. Embossed parallel plates 14. Separator plate

[0041] Figure 3 shows a view of the placement of rockets inside a smart magazine equipped with a precise launch system which contains:

[0042] 1. Rocket 2. Thick rubber belt (conveyor belt)

[0043] 3. The holding base of the system components

[0044] 4. Roller of the conveyor belt

[0045] 5. Smart magazine equipped with precise rocket launch system

[0046] Figure 4 shows the general view of the launch of several rockets on the ice mass.

Claims

What is claimed is:

1. The invention of system of observation and monitoring the earth warming and changes in polar ice behavior using LoRa to satellite technology includes at least one rocket and at least one projectile equipped with three wings and at least one speed limit control umbrella system and at least one incomplete cone and at least one steel rod and at least one separating plate and at least three all-thread rods and at least several parallel raised plates and at least three all-thread wires and at least several plates made of polycarbonate polymer with a circular shape and at least one PCB board or printed circuit fiber and at least one lithium battery and at least one lithium battery charger module and at least several solar cells and at least modules for measuring ice temperature and ambient temperature, air pressure and light intensity and at least one LoRaWAN module and at least one GPS module and at least one magazine for placing rockets and at least one gravity-activated switch.

2. The monitoring system of claim one in which the rocket of the invention is made of a steel cylinder made of 316L steel by rolling method and subpowder welding or argon welding, or made of 316L steel tube with low thickness.

3. The monitoring system of claim one in which the front part of the capsule of the invention, an incomplete cone is formed, which is connected from the base part to the lower part of the cylinder of the capsule by welding method.

4. The monitoring system of claim one in which the incomplete cone is concentric with the cylinder of the capsule and forms the base of the cone at the point of connection with the cylinder of a circular plate.

5. The monitoring system of claim one in which from the upper part of the cone, a steel rod made of anticorrosive mild steel (low-carbon) with weldingcapability comes out, so that the end part of the rod is welded on the plate separating the incomplete cone from the cylinder.

6. The monitoring system of claim one in which the presence of a central hole in the center of the separation plate makes it possible for the ice temperature probe to be placed in the central part of the rod.

7. The monitoring system of claim one in which the three holes on the vertices of an equilateral triangle provide the possibility of screwing three rods of the entire thread, which are designed to hold the internal devices of the electronic mechanism.

8. The monitoring system of claim one in which due to the large diameter of the separating plate of the cylinder and the incomplete cone, it is possible to tap the mentioned holes and create suitable conditions for screwing the mentioned rods inside the separating plate.

9. The monitoring system of claim one in which the middle of the separating plate up to the tip of the incomplete cone is filled with molten lead in such a way that the lead fills the entire inner space of the cone and serves as a support base for the rocket head rod on the one hand and used as a balancer for the rocket weight distribution on the other hand.

10. The monitoring system of claim one in which close to the base of the rod, the presence of parallel raised plates on the rod makes it possible for the molten lead to surround the base of the rod in such a way that it is not possible to separate the lead from the rod.1 l.The monitoring system of claim one in which at the tip of the rod, there is a 60 degree cone with three prominent incomplete cones on the tip of the rod, giving the said rod an arrow shape so that when the rocket hits the ice surface, the rocket can sink into the ice and stabilize the structure of the rocket on the ice.

12. The monitoring system of claim one in which in the inner part of the cylinder, the presence of three fully threaded steel wires makes it possible toplace plates made of polycarbonate polymer with a circular shape and similar concentric holes on these three threaded wires in certain places should be strengthened on the triple rods with a bolts and nut from below and another nut from the other plates.

13. The monitoring system of claim one in which PCB plates or printed circuit board used for internal equipment boards are also in the form of circular plates and generally have a certain thickness, which is placed on polymer plates as a shock absorber support and connections are connected to each other.

14. The monitoring system of claim one in which in the used circuits, only dip parts were used in order to not cause a loss in the performance of the soldering joints due to the impact of thermal and cold hits.

15. The monitoring system of claim one in which the rechargeable lithium batteries section is located on the first floor of the structure, and in order, the ice temperature detection module, then the surrounding air temperature detection module, and then the lithium battery charger module with the help of solar cells, and then the LoRaWAN module for sending and receiving information as well as GPS module is mounted in to extract location and height information.

16. The monitoring system of claim one in which the presence of a narrow ring around the upper part of the cylinder makes it possible for the upper circular plate to be pulled inside the cylinder by tightening its retaining nuts and placed on the step created by the peripheral ring.

17. The monitoring system of claim one in which the existence of three wings in the lower part allows the correct movement of the rocket in the air.

18. The monitoring system of claim one in which the existence of a small fabric umbrella in the lower part caused the mentioned equipment reaches a certain speed while moving in the air, which this terminal velocity is inversely proportional to the cross-sectional area of the said umbrella.

19. The monitoring system of claim one in which the size of the umbrella is adjusted in such a way that the terminal velocity of the said rocket is adjusted in such a way that the inertia of the motion of the rocket of the present invention can sink its rod into the ice and settle on the ice surface when it hits the ice surface.

20. The monitoring system of claim one in which the mentioned rocket is left at its location by a flying device such as a plane, helicopter or balloon.

21. The monitoring system of claim one in which the device of the invention is placed inside a smart magazine equipped with a precise rocket launch system, which consists of two thick rubber belts with an angle equal to the angle of the cone of the rocket head.

22. The monitoring system of claim one in which the rockets are placed on the mentioned conveyor belt and based on the flier coordinates, the height of the device flier from the ice surface and also the topographical map of the ice area, it is moved and released by an artificial intelligence23. The monitoring system of claim one in which at the time of launching each of the rockets, the ring connected to the speed regulating umbrella is outside the end of the rocket, and when the rocket is thrown due to the weight of the rocket, the device moves towards the ground and the speed regulating umbrella comes out from inside the rocket and adjusts the free fall speed of the rocket towards the ground.

24. The monitoring system of claim one in which when the rocket reaches the ground and collides with the ice masses immediately after the first impact, the internal mechanism of the rocket, which is equipped with a gravity- activated key system, starts the process of activating the internal equipment.

25. The monitoring system of claim one in which the entire interior of the rocket has been filled and coated with a flexible composite resin in such a way that when the rocket collides with ice surfaces, it can prevent the transfer of blows to sensitive parts.

26. The monitoring system of claim one in which the outer part of the rocket from the beginning of the top of the middle cone to the halves of the main cylinder of the body is covered with a cover of dense polyurethane foam.

27. The monitoring system of claim one in which the collected information are transferred as the understandable data packets by the LoRaWAN module to a fixed or deployable station with the help of aerial vehicles.

28. The monitoring system of claim one signals are sent by LoRa protocol and commands are also sent from the central station to the satellite or any other transmission and reception structure.

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