A METHOD AND SYSTEM FOR MONITORING THE ASTRONAUT'S HEALTH STATUS.

Abstract

It is concerned with a system (10) and method involving a wearable body to enable the monitoring of the health status of at least one astronaut during a space mission. Figure 1

Description

1 TARIFF A METHOD FOR MONITORING THE ASTRONAUT'S HEALTH STATUS. SYSTEM TECHNICAL FIELD The invention allows for the monitoring of the health status of at least one astronaut during a space mission. It relates to a system and method involving a wearable body to provide this. PREVIOUS TECHNIQUE A space mission is a mission where astronauts conduct scientific research and engineering applications in the space environment. To perform tasks such as station maintenance or exploration activities, in the Earth's atmosphere It is a long-term process during which they are sent outside of their immediate environment. These missions involve zero gravity, radiation, and limited space. physical space, enclosed living environments, and communication restrictions have a direct impact on human health. It contains effective conditions. Therefore, not only are operational goals achieved, at the same time, the uninterrupted physiological and psychological health of the astronauts on duty And reliable protection is also a fundamental requirement for space missions. Prolonged isolation, microgravity conditions, limited living space, and job-related stress. Factors such as these require integrated monitoring and intervention from both physiological and psychological perspectives. This increases the need for these systems. Existing systems mostly only collect data, These are systems that offer limited feedback or require manual intervention. For example... Although current systems can track a great deal of data related to astronauts, based on this data, 25 It does not have the ability to initiate real-time and automated physical intervention. Therefore... together, to protect musculoskeletal health in a zero-gravity environment. The systems used are generally based on large, stationary, and non-wearable devices. This situation restricts astronaut mobility. In addition, in current systems... There are no integrated guidance mechanisms that can offer psychological support. 30 Therefore, problems like stress and loneliness can negatively affect job performance. In conclusion, all the problems mentioned above necessitate an innovation in the relevant technical field. It has made it mandatory. 35 A BRIEF DESCRIPTION OF THE INVENTION 2 The present invention aims to eliminate the aforementioned disadvantages and contribute to the relevant technical field. It is about a system and method aimed at bringing new advantages. One aim of the invention is to monitor the astronaut's physiological data in real time, thereby assessing their health. The goal is to establish a system and method that allows for the monitoring of the situation. 5 Another purpose of the invention is to provide the astronaut with the necessary physical and mental support according to their health condition. The goal is to establish a system and method for providing psychological support. Another aim of the invention is to improve the astronaut's comfort, safety, and 10 during their space mission. personalized and adaptive interventions to improve performance continuity The goal is to establish a system and method that enables its implementation. All the purposes mentioned above and those that will emerge from the detailed explanation below. The current invention aims to achieve this by monitoring the health of at least one astronaut during a space mission. in a system that includes a wearable body to enable monitoring of its condition It is a method to be implemented. Accordingly, the novelty lies in at least one aspect related to the astronaut. At least one physiological sensor from at least one sensing unit that enables the acquisition of physiological data. Data acquisition involves training a team equipped with health status information corresponding to physiological data. Accessing the artificial intelligence model, the aforementioned perception of the mentioned artificial intelligence model 20 By applying at least one physiological data point obtained from the unit, a study was conducted on the aforementioned astronaut. Obtaining health status information as an output, storing health status information in a memory unit Comparison of the available reference health status information with the health status information, It was determined that it matched at least one of the reference health status information mentioned. If necessary, at least one support that provides physical support to the astronaut 25 The operating signal generated for the operation of the unit is sent to the aforementioned support unit. It includes the steps for transmission. Thus, what the astronaut encounters during his space mission... Potential adverse physiological conditions are detected and analyzed in real time. With personalized support applications, the task can be resolved quickly and automatically. Security and quality of life are being improved. 30 A feature of a possible design of the invention is the physiological data received from the sensing unit. This includes the step of recording the astronaut's health status over time. It becomes possible to monitor and analyze individual physiological data. 35 3 Another possible configuration of the invention would feature the astronaut being provided with information about his / her health status. It involves at least one step of transmitting a voice message from a voice-producing unit. Thus Psychological support is provided to the astronaut through soothing audio guidance. Another possible configuration of the invention features a system where, based on health status information, the astronaut is 5 years old. Massage is applied to the astronaut to provide physical support, to strengthen the astronaut's muscles. loosening, lowering the astronaut's body temperature, raising the astronaut's body temperature It should include at least one of these steps. Thus, the astronaut's musculoskeletal health, thermal Task performance and safety are improved by supporting balance and overall body functions. is being increased. 10 Another possible configuration of the invention would feature the astronaut being provided with information about his / her health status. The support unit must be activated to apply massage via at least one massage motor. This involves the step of transmitting the working signal to the support unit. Thus, the astronaut A relaxing and circulation-enhancing intervention targeting the muscular system is provided, long-term 15 Symptoms of muscle tension and fatigue caused by inactivity are minimized. Another possible configuration of the invention would feature the astronaut's health status information. support unit to relax muscles via at least one vibration motor It involves the step of transmitting the operating signal to the support unit for operation. Thus, 20 Muscle stiffness, circulatory problems, and muscle weakness that may occur in a zero-gravity environment Such effects are prevented, and muscle relaxation and function are achieved through low-frequency stimulation. Its continuation is supported. Another possible configuration of the invention features the astronaut being 25 years old, based on information about his health status. Activating the support unit to raise body temperature via at least one heating unit This involves the step of transmitting the operating signal to the support unit. Thus, low temperature The risk of hypothermia caused by space travel is minimized, and the astronaut's thermal comfort is ensured. Maintaining physiological resilience during the mission is supported. Another possible configuration of the invention would feature the astronaut's health status information. support unit to lower body temperature through at least one cooling unit The process involves transmitting the operating signal to the support unit for operation. Thus... decreased performance and thermal effects that may occur due to high body temperature By preventing discomfort, the astronaut's physical and mental competence during the mission is increased by 35. protection is ensured. 4 Another possible configuration of the invention involves performing the above steps within a processing unit. It is carried out by. The invention also allows for the determination of the health status of at least one astronaut during a space mission. and support for the astronaut in question, according to the aforementioned health condition. 5 It relates to a system that includes a wearable body to provide this. Accordingly, its innovation lies in overcoming the previous a processor unit that performs the procedural steps described in the requests It includes. Another possible configuration feature of the invention is that the mentioned body can self-assemble. It is made of materials that can be repaired. Thus, minor damage that may occur in the body can be avoided. The damage can repair itself. Another feature of the invention's possible configuration is that the body is polymer-based self-repairing. It is made of a material that can withstand microscopic damage. Thus, microscopic damage that may occur on the body is prevented. Damage at this level can be automatically repaired thanks to the material's own structure. Another characteristic of the invention's possible construction is that the body is made of nanocomposite material. It is manufactured in such a way that the body combines high mechanical strength and lightness properties. by providing safe use without restricting the astronaut's mobility. 20 It provides. Another possible configuration of the invention features a body made of carbon fiber and titanium. The body is made of alloys, which provides both lightness and high structural integrity. By providing durability, it reduces the burden on the astronaut during space missions while withstanding harsh environments. 25 It is designed to be resistant to these conditions. Another possible configuration of the invention would feature at least one aspect of the body relating to the astronaut. It must contain at least one sensory unit that enables the acquisition of physiological data. Thus The astronaut's real-time health status can be monitored directly through the body. 30 Another possible configuration of the invention would feature at least one of the aforementioned sensing units. It includes a heart rate sensor. Thus, the astronaut's cardiovascular status is monitored in real time. This allows monitoring over time and early detection of potential stress, fatigue, or health risks. It can be detected at this stage. 35 Another possible configuration of the invention features the sensing unit having at least one muscle. It includes a tension sensor. This allows the astronaut's muscle activity to be monitored over a long period. Conditions such as muscle weakness or spasms that may result from inactivity can be prevented. It can be determined. Another possible configuration of the invention features a sensing unit with at least one thermal element. It includes a sensor. Thus, the astronaut's body temperature is continuously monitored, and sudden changes are detected. It can be detected. Another possible configuration of the invention features a sensing unit with at least one galvanic 10 It includes a skin response sensor. Another possible configuration feature of the invention is that the body would physically support the astronaut. It must include at least one support unit that provides support. Thus, the astronaut's needs are met. The physical support they need is provided immediately, increasing their comfort. 15 Another possible configuration of the invention involves the aforementioned support unit providing the astronaut with... It must include at least one massage motor to administer a massage. This allows the astronaut to... Relaxation is achieved by reducing tension in the muscles. Another possible configuration of the invention features a support unit that would support the astronaut's muscles. It includes at least one vibration motor to relax the muscles. Thus, muscle tension is reduced. Circulation is supported and muscle function is preserved. Another possible configuration of the invention features a support unit that attaches to the astronaut's body 25 It must include at least one heating unit to increase its heat. Thus, low temperature sources The risk of hypothermia is reduced. Another possible configuration of the invention features a support unit attached to the astronaut's body. It must include at least one cooling unit to reduce its temperature. Thus, the risk of overheating is reduced to 30. By reducing the amount of heat, the astronaut's thermal comfort and performance are preserved. Another possible configuration of the invention features a body that could deliver an audio message to the astronaut. It must contain at least one sound-producing unit for transmission. 35 6 BRIEF DESCRIPTION OF THE FIGURE Figure 1 shows a representative view of the system. DETAILED DESCRIPTION OF THE INVENTION 5 This detailed explanation of the invention does not merely aim to improve understanding of the subject matter; it does not contain any other information. This is explained with examples that will not create a limiting effect. Referring to Figure 1, the invention suggests that the health status of at least one astronaut during a space mission will be 10 a system (10) and method that includes a wearable body to enable it to be controlled is related. The mentioned system (10) and method are related to the astronaut's space mission. supporting the astronaut in the face of any physical or psychological challenges they may encounter. It provides. In a possible configuration of the invention, the wearable body described would be attached to the astronaut's body. It can be designed to make contact with the body. Accordingly, it can be designed for the torso, shoulders, back, and head area. It has a wearable ergonomic design. Thanks to its lightweight and modular structure, it fits different body types. It adapts to the dimensions and allows for long-term use without restricting mobility. It offers support. 20 In a possible configuration of the invention, the body would be made of self-repairing materials. It may be manufactured. Thus, the system (10) can be manufactured under long-term operational conditions. ensuring its integrity and functionality without the need for external intervention. This prevents malfunctions. This structure reduces the need for maintenance and is especially important in space. 25 In situations where repair options are limited in the environment, the system's robustness and This increases the reliability of the task. Self-repairing materials in technology. Since this was already known, no further explanation was given. In a possible configuration of the invention, the body would be a polymer-based, self-repairing 30 It may be manufactured from a specific material. The aforementioned polymer-based materials are well-suited to the technology. As is known, their lightness and shape conformity make them ideal for wearable bodies, thus improving ergonomics. Furthermore, polymer-based materials withstand temperature variations in the space environment and By maintaining its flexibility in the face of mechanical stresses, it both increases user comfort. and also maintains the structural integrity of the fuselage. 35 7 In a possible configuration of the invention, the body is made of nanocomposite material. This is possible. As is well known in the field of technology, the aforementioned nanocomposite materials have high... by offering features such as mechanical strength, low weight and resistance to environmental effects This type of material supports both the robustness and long-lasting use of the housing. The materials inhibit crack propagation thanks to microscopically dispersed admixtures. slowing down and preserving structural integrity the system may encounter in space missions. It increases its resistance to thermal, mechanical, and radiation-induced stresses. This will minimize both the functionality of the body and the burden on the astronaut. It is possible to optimize it in this way. In a possible design of the invention, the fuselage would be manufactured from carbon fiber and titanium alloys. It may have been done. The aforementioned carbon fiber and titanium alloys are well known in the field. Thanks to its high strength-to-weight ratio, it is both a durable and lightweight structure. This allows the body to support the astronaut for extended periods without limiting their mobility. These materials are becoming suitable for use. Furthermore, these materials can withstand the extreme conditions encountered in the space environment. structural integrity in the face of temperature differences, vibrations and mechanical stresses By protecting it, it increases the reliability and continuity of the system throughout its operational lifespan. The system has (10) bodies that enable at least one physiological data point to be obtained about the astronaut. It includes a sensing unit (11). Through the aforementioned sensing unit (11), for example 20 physiological parameters related to the astronaut such as heart rate, muscle activity, body temperature, or stress level It enables the real-time measurement of parameters. In this way, the system (10), We can monitor changes in the astronaut's health status in real time and, if necessary... It supports physiological balance by activating appropriate responses. In a possible configuration of the invention, the mentioned sensing unit (11) is the heart of the astronaut. It includes at least one heart rate sensor that allows for measuring heart rate. (mentioned) The heart rate sensor continuously monitors data regarding the astronaut's cardiovascular system. By monitoring, we can detect abnormalities in the heartbeat and assess the astronaut's health status. This allows for evaluation accordingly. Sudden changes in heart rate, stress, 30 Because this data can be an early sign of conditions such as fatigue or circulatory problems, It plays a critical role in monitoring the astronaut's overall health. In a possible configuration of the invention, the sensing unit (11) would detect the muscle activity of the astronaut. It includes at least one muscle tension sensor for measurement. The muscle tension mentioned is 35. The sensor monitors tension levels in the muscles, determining the astronaut's muscle activity and fatigue. It allows for the detection of the level or possible muscle strains. In particular 8 risk of muscle weakness that may result from prolonged immobility in a weightless environment This is important because it provides early warning. In this way, the system monitors muscle health. They can initiate protective interventions in a timely manner. In a possible configuration of the invention, the sensing unit (11) would measure the astronaut's body temperature at 5°C. It includes at least one thermal sensor to enable measurement. The aforementioned thermal sensor, By continuously monitoring the astronaut's body temperature, potential heat balance disorders can be detected early. It can detect this in stages. Sudden temperature changes in the space environment or during the mission Conditions such as infection, fatigue, or overexertion that may occur during this time can affect the body. Because it can affect temperature, monitoring this data is important for the astronaut's overall health. It provides important information about the situation. In a possible configuration of the invention, the sensing unit (11) shall have at least one galvanic skin response. It includes a sensor. The aforementioned galvanic skin response sensor monitors the astronaut's skin. By measuring changes in electrical conductivity on its surface, it can detect stress, anxiety, or emotional disturbances. It can indirectly detect situations such as arousal. Early detection of psychological stress. to determine, monitor the astronaut's mental state during the mission and, if necessary It offers significant advantages in terms of initiating supportive interventions. The system includes (10) bodies, at least one support that provides physical support to the astronaut 20 It includes support unit (13). The aforementioned support unit (13) is used to support the astronaut during the mission. directly against conditions such as muscle tension, immobility, and feelings of cold that it may encounter. It aims to provide physical relaxation. Massage, heating / cooling, or muscle relaxation. This unit, which can undertake functions such as those specified by the system (10), according to the needs determined by the system (10). 25 that are automatically activated to help maintain the astronaut's physiological balance is happening. In a possible configuration of the invention, the support unit (13) is designed to apply massage to the astronaut. It includes at least one massage motor. The aforementioned massage motor produces vibrations. They may include piezoelectric elements or micro electromechanical motors. Accordingly, 30 By sending rhythmic stimuli to targeted body areas, it relaxes muscles and increases blood flow. It helps to support circulation. The massage motor is especially useful for relieving muscle tension or Helps alleviate physical discomfort that can be caused by prolonged immobility. This is achieved through vibration-based massage applied to targeted body areas. This helps relax the muscles, supports circulation, and improves the astronaut's overall physical condition. Comfort is increased. This prevents performance loss during long-term tasks. 9 In a possible configuration of the invention, the support unit (13) would relax the astronaut's muscles. It includes at least one vibration motor. The aforementioned vibration motor is low-frequency. By mimicking muscle activity through stimuli, it causes muscles to relax and relieves tension caused by inactivity. It helps to reduce the voltage. Also, the support unit (13), Electromyostimulation (EMS) technology stimulates muscles directly with electrical signals. 5 It can stimulate muscle tissue, thereby keeping it active through these stimuli and ensuring long-term protection. It helps prevent muscle weakness and bone mineral loss caused by inactivity. This structure prevents musculoskeletal disorders that may occur in a weightless environment. It offers effective support for reducing [the disease]. In a possible configuration of the invention, the support unit (13) would increase the astronaut's body temperature. It includes at least one heating unit. The aforementioned heating unit has low environmental impact. to prevent the negative effects that high temperatures could have on the astronaut's body temperature It can be operated for this purpose. The heating unit uses heating elements such as thin-film resistors. or may include micro-heating surfaces. This allows the 15 inches of the astronaut's body to be heated. By increasing the temperature in these areas, thermal comfort is improved. Thus, the risk of hypothermia is reduced. is being monitored and both the physiological and mental performance of the astronaut during the mission is being assessed. This contributes to its protection. In a possible configuration of the invention, the support unit (13) would reduce the astronaut's body temperature. It includes at least one cooling unit. The aforementioned cooling unit is used during duty. potential excessive exertion, equipment-generated heat buildup, or increases in ambient temperature In situations like these, it helps the astronaut regulate their body temperature. The invention is possible. a cooling unit in a configuration, liquid-cooled microchannel systems or thermoelectric It can provide local or general cooling using (Peltier) modules. Thus, excessive 25 to prevent physical discomfort and decreased performance that may be caused by overheating It is being passed. In a possible configuration of the invention, the support unit (13) transmits an audio message to the astronaut. It contains at least one sound reproduction unit (14). The aforementioned sound reproduction unit (14) is 30 It enables the transmission of the generated voice messages. For this purpose, the voice generating unit (14) ensures the transmission of the generated voice messages. It may include a small number of speakers. The system (10) includes a processing unit (15) for monitoring the astronaut's health status. It includes. In a possible configuration of the invention, the processor unit mentioned (15) is a CPU, 35 This could be a GPU, a microprocessor, etc. The processing unit (15) has at least one physiological sensor from at least one sensing unit (11) relating to the astronaut. It enables the acquisition of data. The invention is mentioned in a possible configuration. physiological data includes the astronaut's heart rate, muscle tension, body temperature, and galvanic skin. This data may include at least one physiological parameter, such as the astronaut's response. 5. Assessment of health status, stress level, or physical exertion It provides. The processing unit (15) is trained with health status information corresponding to physiological data. It enables access to an artificial intelligence model. The processor unit (15) provides access to the aforementioned artificial intelligence model. By applying at least one physiological data from the perception unit (11) to the intelligence model, 10 It provides output of information regarding the astronaut's health status. In a possible configuration of the invention, information on health status, including the astronaut's normal, borderline, or moderate health, would be required. or whether they are in a physiological condition that could be classified as risky It can include, for example, an increase in heart rate, increased muscle tension, and body 15 Data such as a decrease in temperature or the galvanic skin response exceeding certain thresholds are artificial. The intelligence model describes "high stress level," "overexertion," "low thermal comfort," or "muscle" It can also produce output of health status information such as "fatigue". Furthermore, it can also generate health status information. This information may also include details such as the need for relaxation or a possible fainting spell. The processor unit (15) stores the health status information in a memory unit (12) containing reference health information. It allows comparison with the information regarding the situation. In a possible configuration of the invention. Reference health status information stored in the aforementioned memory unit (12), in advance defined threshold values, astronaut-specific biometric profiles, or mission environment-specific criteria. It can include adapted health criteria. Thus, the system (10) detects any deviation or 25 when a risky situation is identified, the necessary interventions should be started without delay. It provides. The reference health status mentioned in a possible configuration of the invention. information, high stress level, overexertion, low thermal comfort, muscle fatigue, relaxation It may include information such as the need or possible state of fainting. A possible invention... In its structure, the memory unit (12) stores data permanently and temporarily when needed. It can include a combination of memory types that also store information. The processing unit (15) provides health status information at least from the reference health status information. If it is determined that the astronaut is physically identical to someone else, A study to ensure that at least one support unit (13) is operational to support it. 35 It enables the generation of a signal. The aforementioned signal is a health status signal. in cases where the information matches predefined reference thresholds 11 This is possible. This ensures that intervention is timely and targeted. is provided. The processor unit (15) transmits the mentioned operating signal to the support unit (13). Thus, the support unit (13) is put into operation as a result of the evaluation and 5 The necessary intervention procedures are being initiated. In a possible configuration of the invention, the processor unit (15) is based on health status information. Administering a massage to the astronaut to provide physical support to the astronaut, relaxing the muscles, lowering or raising the astronaut's body temperature 10 It provides. In a possible configuration of the invention, the processor unit (15) is the health of the support unit (13). According to the information available, the astronaut should be given a massage using at least one massage motor. Massage helps reduce muscle tension, improve circulation, and provides long-term relief. to prevent physical discomfort caused by prolonged inactivity is initiated. For example, the muscle tension sensing unit in the astronaut's shoulder region (11) when detected by and this status information is recorded as "high muscle" It can be classified as "tension". Accordingly, the processor unit (15) responds to this information. It can operate the massage motor located in the shoulder area. Therefore, the massage 20 the motor, typically applied to larger surface areas, applies physical pressure to the tissue. and provides rhythmic vibration. In a possible configuration of the invention, the processor unit (15) is the health of the support unit (13). According to the information on the situation, the astronaut's muscles were being stimulated by at least one vibration motor for 25 minutes. It allows for relaxation. The aforementioned vibration motor provides lower amplitude and specific vibrations. micro-operations that target specific muscle groups directly, operating within certain frequency ranges. It is a device that mimics muscle activity through vibrations. The vibration motor causes local muscle relaxation. while providing relief, it is especially beneficial for muscle fatigue, strain, or inactivity. It helps to reduce strain. For example, "muscle tension" or "physical stress". When health status information is obtained, the vibration motor directs a low pressure to the target muscle area. It involves applying high-frequency vibrations. This application causes relaxation in the muscle tissue. By creating this effect, it both supports circulation and helps relieve prolonged immobility. It helps prevent muscle strains that may result from injury. 35 In a possible configuration of the invention, the processor unit (15) is based on health status information. support unit (13) through at least one cooling unit the astronaut’s body temperature 12 This helps to reduce [excessive body temperature] or [low thermal comfort]. When this health status information is obtained, the cooling unit cools the astronaut's body. It helps to lower the body temperature. This prevents fatigue caused by overheating. Negative effects such as decreased performance or circulatory problems can be prevented. In a possible configuration of the invention, the processor unit (15) is based on health status information. The support unit (13) can raise the astronaut's body temperature through at least one heating unit. It enables the improvement of health status information, for example, low body temperature. If hypothermia is identified as a lack of thermal comfort, the heating unit will be turned away from the astronaut. It causes an increase in body temperature. This, in turn, slows circulation and reduces muscle control. Physiological risks associated with hypothermia, such as cognitive impairment and decreased performance, are reduced. In a possible configuration of the invention, the processor unit (15) is based on health status information. It ensures that at least one voice message is transmitted to the astronaut from the voice transmission unit (14). In this way, the processing unit (15) can send voice messages to the astronaut in accordance with the determined health status information. It can convey warnings, information, or guidance. For example, "high stress level". When detected, audio messages with relaxing, guiding and calming content are provided. The astronaut's psychological state is stabilized. This allows them to perform their mission successfully. maintaining mental resilience and sustaining individual focus throughout the period An important support mechanism is offered in this regard. 20 In a possible configuration of the invention, the system (10) takes into account the psychological state of the astronaut. It may include a virtual coaching feature to provide support. Accordingly, the astronaut Motivation based on parameters such as experience, length of service, and individual background. Enhancement feedback and guiding audio content can be provided. The system has (10) processors 25 The unit (15) also includes familiar smells to the astronaut in order to reduce sensory overload, an alternate environment simulated through visual elements or tactile stimuli It can create. For this purpose, the system (10) requires a display unit and an interface. It may include. In a possible configuration of the invention, the aforementioned interface and screen It can be a mobile application accessed via this means. 30 This makes it easier for the astronaut to adapt to their mission location. In a possible configuration of the invention, the processor unit (15) receives from the sensing unit (11). It enables the recording of physiological data. This allows for the astronaut's health history to be compiled. 35 It can be created. Through this data accumulated over time, the system (10) enables the user They can learn about individual physiological responses and make better assessments of their health status. 13 This enables the support units to achieve more accurate response levels. Thus, the working thresholds of the support units and the intervention levels can be adjusted. Timings and priority levels are optimized according to the astronaut's individual physiological characteristics. This provides a more effective and adaptable support process. In a possible configuration of the invention, the movement exhibited by the astronaut during the mission is 5 By learning about their behaviors and physiological responses over time, they can adapt their support strategies accordingly. It can adapt the processor unit (15) to repetitive muscle activity or a specific movement. by identifying potential muscle strains that may occur as a result of frequent use and providing the necessary support in advance. It can take preventive action by enabling the operation of the unit (13). In a possible configuration of the invention, the processor unit (15) is a long-term or permanent space in their missions, geared towards the personal needs of the astronaut at a specific place or time It can artificially simulate sensory characteristics. This includes the astronaut's vision, Perceptual reconstruction of the targeted environment through senses such as hearing, touch, and smell. This ensures the production of [product / service]. Thus, psychological distress is prevented and emotional balance is maintained. 15 It is protected. For example, it represents a home environment for an astronaut on a long-term mission. a calming scene, for example, the setting of a dinner spent with family members This can be simulated by the system through sensory data. A sample working scenario for the invention is given below; 20 An astronaut is able to perform routine equipment checks inside the space station. Meanwhile, the system (10) worn by the astronaut detects the astronaut's heartbeat through its sensing units. An increase in heart rate, increased muscle tension, and decreased body temperature were detected. It can be done. Physiological data received from the sensing unit (11) are processed by the processing unit (15) artificial 25 This is applied to the intelligence model. As a result of the analysis, the astronaut's health status is determined to be "moderate". These can be classified as "high level of physical stress" and "low thermal comfort". The processor unit (15) stores the obtained health status information in the memory unit (12). It can determine if the information matches by comparing it with reference health status information. 30 In this respect, the processor unit (15) generates an operating signal, and the support units It enables it to work automatically. For example, a vibration motor for this purpose, targeting the relevant muscle. While generating low-frequency stimuli to promote relaxation in the groups; the heating unit, It can provide local heat to regulate body temperature. It also produces sound. A short, calming voice guidance message is also sent to the astronaut via unit (14) 35 It can be transmitted. 14 All physiological data obtained during this support process is recorded and the astronaut's Individual behaviors are analyzed by the processing unit (15). Thus the system (10) will respond faster and more effectively when faced with similar situations. This allows for the adaptation of support strategies. This structure is based on continuous learning. Thanks to this system, the astronaut's physical and psychological well-being is monitored throughout their mission. Personalized solutions are offered to help maintain balance. The scope of protection of the invention is specified in the claims attached hereto, and these details are strictly adhered to. The explanation cannot be limited to those given for illustrative purposes. Because a technically skilled person... The person, without deviating from the main theme of the invention, can create similar 10 based on the above-mentioned points. It is clear that these structures can emerge. REFERENCE NUMBERS GIVEN IN THE FIGURE System 11 sensing units 12 Memory units 5 13 Support Units 14 Sound reproduction units Processor unit

Claims

16 REQUESTS 1. Checking the health status of at least one astronaut during the space mission. to be performed in a system that includes a wearable body (10) in order to provide It is a method and its characteristic is; 5 - at least one piece of physiological data relating to the astronaut that enables the collection of at least one piece of data. Obtaining at least one physiological data from the sensing unit (11), - trained with health status information corresponding to physiological data Access to the artificial intelligence model, - 10 taken from the mentioned sensing unit (11) to the mentioned artificial intelligence model By applying at least one physiological data point, a study was conducted on the astronaut in question. Obtaining health status information as a printout. - reference health status information located in a memory unit (12) Comparing the situation with the information, - health status information 15% of the aforementioned reference health status information. If at least one of them is found to be the same, the astronaut at least one support unit that provides physical support (13) the operating signal generated for its operation is sent to the aforementioned support unit. (13) transmission, It includes the steps. 20 2. It is a method according to claim 1 and its feature is; physiological data obtained from the sensing unit (11). This includes the step of recording the data.

3. A method according to Claim 1, characterized by its ability to provide the astronaut with at least 25 days of medical care based on health status information. It involves the step of transmitting an audio message from a small sound-producing unit (14).

4. It is a method according to Claim 1, characterized by its ability to assess the astronaut's health status. Administering a massage to the astronaut to provide physical support, the astronaut relaxing the muscles, lowering the astronaut's body temperature, lowering the astronaut's body 30 It involves at least one of the steps to increase its temperature.

5. It is a method according to Claim 1, characterized by its ability to provide the astronaut with the best possible health status information. Support unit (13) 35 for applying massage via a small massage motor the step of transmitting the operating signal to the support unit (13) for operation It includes. 17 6. This is a method according to Claim 1, characterized by its ability to assess the astronaut's health status. support unit (13) to relax your muscles via a small vibration motor the step of transmitting the operating signal to the support unit (13) for operation It includes.

7. It is a method according to Claim 1, characterized by its ability to assess the astronaut's health status. support unit (13) to increase body temperature through a small heating unit the step of transmitting the operating signal to the support unit (13) for operation It includes.

8. This is a method according to Claim 1, characterized by its ability to assess the astronaut's health status. support unit (13) to lower body temperature through a small cooling unit the step of transmitting the operating signal to the support unit (13) for operation It includes.

9. It is a method according to claim 1 and its feature is that the above steps are performed by a processor unit (15) It is carried out by.

10. To ensure that the health status of at least one astronaut is determined during the space mission, and 20 to ensure that the aforementioned astronaut receives support according to the aforementioned health condition a system (10) which includes a wearable body for; its feature is; in previous requests a processor unit (15) that is used to perform the described method steps It includes.

11. According to claim 10, a system (10) has the characteristic that the mentioned body self-regulates 25 It is made of materials that can be repaired.

12. A system (10) according to claim 10, whose characteristic is that the body is polymer-based self-repairing. It is made of a material that can withstand such conditions.

13. A system (10) according to claim 10, whose characteristic is that the body is made of nanocomposite material. It is the fact that it has been manufactured.

14. A system (10) according to claim 10, whose characteristic is that the fuselage is made of carbon fiber and titanium. It is made of alloys. 35 15. A system (10) according to claim 10, and its characteristic is that the body has at least one astronaut-related feature. It includes at least one sensing unit (11) that enables the acquisition of physiological data. 18 16. According to claim 15, a system (10) is characterized by the fact that the mentioned sensing unit (11) is the most It includes a small heart rate sensor.

17. According to claim 15, a system (10) has the characteristic that the sensing unit (11) has at least one muscle It includes a tension sensor. 5 18. A system (10) according to claim 15 has the characteristic of having at least one thermal sensing unit (11). It includes a sensor.

19. According to claim 15, a system (10) has the characteristic that the sensing unit (11) has at least one 10 It includes a galvanic skin response sensor.

20. A system (10) according to claim 10, whose characteristic is that the body is physically positioned so that the astronaut can be placed inside it. It includes at least one support unit (13) that enables it to be supported.

21. According to claim 20, a system (10) and its feature is; the mentioned support unit (13), It should include at least one massage motor to provide massage to the astronaut.

22. According to claim 20, a system (10) is characterized by; the support unit (13), the astronaut It includes at least one vibration motor to relax the muscles. 20 23. According to claim 20, a system (10) is characterized by; the support unit (13), the astronaut It must include at least one heating unit to raise body temperature.

24. According to claim 20, a system (10) is characterized by; the support unit (13), the astronaut 25 It must include at least one cooling unit to lower body temperature.

25. A system (10) according to claim 15, whose characteristic is that the body delivers an audio message to the astronaut. It must contain at least one sound transmission unit (14) for transmission.