Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations

Under extreme accelerations, human physiological mechanisms cannot provide adequate circulation. Special methods and devices protecting pilot’s brain and eye functionality have been proposed but their efficiency is individual and depends on pilot’s skills. Currently, the lonely technology to safely...

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Автор: Grygoryan, R.D.
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Опубліковано: Інститут програмних систем НАН України 2024
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spelling pp_isofts_kiev_ua-article-6042024-04-27T17:04:37Z Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations Проблеми створення спеціального програмного забезпечення для моделювання фізіологічних реакцій людини на динамічні прискорення Grygoryan, R.D. human extreme physiology; quantitative models; simulator; training; information technology UDC 517.958:57 +519.711.3 + 612.51.001 екстремальна фізіологія людини; кількісні моделі; тренажер; навчання; інформаційна технологія УДК 517.958:57 +519.711.3 + 612.51.001 Under extreme accelerations, human physiological mechanisms cannot provide adequate circulation. Special methods and devices protecting pilot’s brain and eye functionality have been proposed but their efficiency is individual and depends on pilot’s skills. Currently, the lonely technology to safely acquire and test the necessary skills is based on use of special centrifuges. However, lack of adequate data about physiological and biomechanical events are two main causes worsening the training results. Special computer simulators, capable to model and visualize the main mechanical and physiological effects occurring under dynamic accelerations, could increase the effectiveness of future pilot’s training process. This publication aims to define fundamental problems concerned with creating the required software. There exist two main groups of problems. The first group is concerned with the necessity to create basic mathematical models quantitatively describing both the physiological events and effects induced by protective maneuvers. Here special logical procedures, individualizing the basic physiological models, have to be proposed. The second group of problems is predominantly technical and associated with the necessity of special user interface (SUI) development. SUI must be subdivided into two functional sections – one for preparing a single computer experiment (simulation), and another – for analyzing the results of simulation. An experiment preparation includes the following events: i) a preliminary tuning of models according to biometrical data; ii) a setting of acceleration profile; iii) a choosing of protective algorithms and tools (or without protections); iv) a choosing of forms for results storage. Graphs presenting the dynamics of input and output variables are the main forms while the table forms are also included. The user (trainer or trainee) will be able to retrieve from the memory graphs of previous simulations to compare the effectiveness of additional protective elements. The software must be autonomic for the Windows platform.Prombles in programming 2024; 1: 30-37 Під час екстремальних прискореннях фізіологічні механізми людини не можуть забезпечити належний кровообіг. Були запропоновані методи та пристрої для захисту мозку та очей пілота. Їхня ефективність індивідуальна і залежить від навичок пілота. Наразі єдина технологія безпечного отримання та перевірки необхідних навичок базується на використанні спеціальних центрифуг. Однак відсутність адекватних даних про фізіологічні та біомеханічні події є двома основними причинами погіршення результатів тренувань. Підвищити ефективність процесу підготовки майбутнього пілота могли б спеціальні комп’ютерні тренажери, здатні моделювати та візуалізувати основні механічні та фізіологічні ефекти, що виникають у випадку динамічних прискорень. Ця публікація має на меті визначити фундаментальні проблеми, пов’язані зі створенням необхідного програмного забезпечення. Існує дві основні групи проблем. Перша група пов’язана зі створенням базових математичних моделей, які кількісно описують фізіологічні події та ефекти, спричинені захисними маневрами. Тут повинні бути запропоновані спеціальні логічні процедури, що індивідуалізують основні фізіологічні моделі. Друга група проблем має переважно технічний характер і пов’язана з необхідністю розробки спеціального інтерфейсу користувача (СІК). СІК необхідно розділити на дві функціональні частини – першу для підготовки одного комп’ютерного експерименту (моделювання), а другу – для аналізу результатів моделювання. Підготовка експерименту включає наступні заходи: i) попереднє налаштування моделей за біометричними даними; ii) налаштування профілю прискорення; iii) вибір захисних алгоритмів та інструментів (або без захисту); iv) вибір форм для зберігання результатів. Графіки, що представляють динаміку вхідних і вихідних змінних, є основними формами, а табличні форми також включені. Користувач (тренер або стажер) зможе отримати з пам’яті графіки попередніх симуляцій для порівняння ефективності додаткових захисних елементів. Програмне забезпечення має бути автономним для платформи Windows.Prombles in programming 2024; 1: 30-37 Інститут програмних систем НАН України 2024-04-01 Article Article application/pdf https://pp.isofts.kiev.ua/index.php/ojs1/article/view/604 10.15407/pp2024.01.030 PROBLEMS IN PROGRAMMING; No 1 (2024); 30-37 ПРОБЛЕМЫ ПРОГРАММИРОВАНИЯ; No 1 (2024); 30-37 ПРОБЛЕМИ ПРОГРАМУВАННЯ; No 1 (2024); 30-37 1727-4907 10.15407/pp2024.01 en https://pp.isofts.kiev.ua/index.php/ojs1/article/view/604/654 Copyright (c) 2024 PROBLEMS IN PROGRAMMING
institution Problems in programming
baseUrl_str https://pp.isofts.kiev.ua/index.php/ojs1/oai
datestamp_date 2024-04-27T17:04:37Z
collection OJS
language English
topic human extreme physiology
quantitative models
simulator
training
information technology
UDC 517.958:57 +519.711.3 + 612.51.001
spellingShingle human extreme physiology
quantitative models
simulator
training
information technology
UDC 517.958:57 +519.711.3 + 612.51.001
Grygoryan, R.D.
Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations
topic_facet human extreme physiology
quantitative models
simulator
training
information technology
UDC 517.958:57 +519.711.3 + 612.51.001
екстремальна фізіологія людини
кількісні моделі
тренажер
навчання
інформаційна технологія
УДК 517.958:57 +519.711.3 + 612.51.001
format Article
author Grygoryan, R.D.
author_facet Grygoryan, R.D.
author_sort Grygoryan, R.D.
title Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations
title_short Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations
title_full Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations
title_fullStr Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations
title_full_unstemmed Problems associated with creating special software for simulating of human physiological responses to dynamic accelerations
title_sort problems associated with creating special software for simulating of human physiological responses to dynamic accelerations
title_alt Проблеми створення спеціального програмного забезпечення для моделювання фізіологічних реакцій людини на динамічні прискорення
description Under extreme accelerations, human physiological mechanisms cannot provide adequate circulation. Special methods and devices protecting pilot’s brain and eye functionality have been proposed but their efficiency is individual and depends on pilot’s skills. Currently, the lonely technology to safely acquire and test the necessary skills is based on use of special centrifuges. However, lack of adequate data about physiological and biomechanical events are two main causes worsening the training results. Special computer simulators, capable to model and visualize the main mechanical and physiological effects occurring under dynamic accelerations, could increase the effectiveness of future pilot’s training process. This publication aims to define fundamental problems concerned with creating the required software. There exist two main groups of problems. The first group is concerned with the necessity to create basic mathematical models quantitatively describing both the physiological events and effects induced by protective maneuvers. Here special logical procedures, individualizing the basic physiological models, have to be proposed. The second group of problems is predominantly technical and associated with the necessity of special user interface (SUI) development. SUI must be subdivided into two functional sections – one for preparing a single computer experiment (simulation), and another – for analyzing the results of simulation. An experiment preparation includes the following events: i) a preliminary tuning of models according to biometrical data; ii) a setting of acceleration profile; iii) a choosing of protective algorithms and tools (or without protections); iv) a choosing of forms for results storage. Graphs presenting the dynamics of input and output variables are the main forms while the table forms are also included. The user (trainer or trainee) will be able to retrieve from the memory graphs of previous simulations to compare the effectiveness of additional protective elements. The software must be autonomic for the Windows platform.Prombles in programming 2024; 1: 30-37
publisher Інститут програмних систем НАН України
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fulltext Прикладне програмне забезпечення 30 УДК 517.958:57 +519.711.3 + 612.51.001 http://doi.org/10.15407/pp2024.01.30 R.D. Grygoryan PROBLEMS ASSOCIATED WITH CREATING SPECIAL SOFTWARE FOR SIMULATING OF HUMAN PHYSIOLOGICAL RESPONSES TO DYNAMIC zG ACCELERATIONS Under extreme accelerations, human physiological mechanisms cannot provide adequate circulation. Special methods and devices protecting pilot’s brain and eye functionality have been proposed but their efficiency is individual and depends on pilot’s skills. Currently, the lonely technology to safely acquire and test the nec- essary skills is based on use of special centrifuges. However, lack of adequate data about physiological and biomechanical events are two main causes worsening the training results. Special computer simulators, ca- pable to model and visualize the main mechanical and physiological effects occurring under dynamic accel- erations, could increase the effectiveness of future pilot’s training process. This publication aims to define fundamental problems concerned with creating the required software. There exist two main groups of prob- lems. The first group is concerned with the necessity to create basic mathematical models quantitatively de- scribing both the physiological events and effects induced by protective maneuvers. Here special logical procedures, individualizing the basic physiological models, have to be proposed. The second group of prob- lems is predominantly technical and associated with the necessity of special user interface (SUI) develop- ment. SUI must be subdivided into two functional sections – one for preparing a single computer experiment (simulation), and another – for analyzing the results of simulation. An experiment preparation includes the following events: i) a preliminary tuning of models according to biometrical data; ii) a setting of accelera- tion profile; iii) a choosing of protective algorithms and tools (or without protections); iv) a choosing of forms for results storage. Graphs presenting the dynamics of input and output variables are the main forms while the table forms are also included. The user (trainer or trainee) will be able to retrieve from the memory graphs of previous simulations to compare the effectiveness of additional protective elements. The software must be autonomic for the Windows platform. Keywords: human extreme physiology, quantitative models, simulator, training, information technology. Introduction Maneuvers on modern fighter aircraft are associated with rapid altering and often highly sustained extreme accelerations [1-3]. Both physiological [4-9] and biotechnical [10- 12] problems that arose in parallel with an increase in military aircraft's maneuverability have been properly investigated [4-18]. Hu- man physiology evolutionarily adapted to the one g Earth environment, cannot provide ade- quate functioning of the brain and eyes of a sitting person. Two of these organs, very sen- sitive to oxygen and glucose supply, suffer in parallel with the decreasing of their input blood pressure. Under accelerations, the hy- drostatic pressure proportional to the accelera- tion value expands the vascular wall, accumu- lating greater blood volume. The altered pres- sure gradients do not provide the necessary circulation at the cardiovascular scale. Accel- erations also alter the ventilation-perfusion ratio in lungs [13,14]. Most critical are positive (+Gz) accel- erations acting in the direction of head-legs, or negative (-Gz) accelerations acting in the opposite direction [4-6]. In terminal zones (brain, eyes), the lowered circulation causes oxygen lack and worsens the pilot’s vision and consciousness [9,12]. Under -Gz, the ele- vated local blood pressure in the eyes and brain causes rupture of microscopic vessels and hemorrhages. Both the value of Gz and the gradient of acceleration change play an essential role in these events. Under relatively slow (0.1-0.4 g/sec) linearly increasing +Gz accelerations, a mean healthy person not using artificial protections is operable for approximately +4Gz accelera- tions [11]. Further elevation of the G-load causes the G-lock phenomenon usually disap- pearing after a break [2,6,8]. Modern fighter aircrafts (like F16, F35, and others) can provide acceleration gra- © R.D. Grygoryan, 2024 ISSN 1727-4907. Проблеми програмування. 2024. №1 Прикладне програмне забезпечення 31 dients exceeding 2 g/sec. This requires special protection algorithms and devices. Currently, typical protection algorithms include the use of special pneumatic or water-augmented an- ti-G suits, muscle stress, as well as breathing with a positive pressure air [1,11,17]. The adaptive protection algorithms combining multiple methods depending on the dynamics of accelerations are the most effective. So, a technology helping to optimally combine pro- tective methods and tools is encouraged. Traditionally, empiric research on cen- trifuges is the main way for inventing more effective protections [1,5,6-8]. As was demonstrated in [18-20], mathematical mod- els realized as special software provided by additional ways to maximize the individual resistance of a pilot to the negative effects of accelerations. The experience in this special area is a basis for creating an advanced ver- sion of such software. This article defines the main require- ments for future software and ways for its creation. Main functional blocks of the future software 1. The main blocks of models The main mathematical models conven- tionally divided into two groups are shown in Fig.1. Figure1. Mathematical models and procedures to be used in the future software. Fig.1 indicates that there should be cre- ated two blocks of quantitative models: mod- els of physiological mechanisms; and models representing environmental physical factors modulating local, regional, or total hemody- namics. Models of physiological mechanisms should quantitatively describe the dynamics of blood pressures, volumes, and flows of a sitting person under altering blood hydrostatic pressure. Important is that the model must describe the main neural-hormonal influences (modulations) of characteristics, involved in descriptions of both the cardiac pump func- tion and vascular tonus. A correct understanding of the student (future pilot) of the essence of physiological processes during flight overloads can play an essential role in the acquisition of profession- al skills. Usually, empirical technologies for training pilots to counteract the undesirable effects of g-forces focus on two main circum- stances caused by extreme accelerations: 1) narrowing of the field of peripheral vision or loss of vision; 2) loss of consciousness as an extreme manifestation (G-lock). These phe- nomena, caused by a deterioration of the eyes and brain oxygen supply, are only manifesta- tions of more extensive changes in human hemodynamics. However, empirics provide very scant information about these hemody- namic processes. The matter is that standard measurements are limited to monitoring the dynamics of heart rate (HR) and blood pres- sure. The shift in HR can be provided by multiple mechanisms. Several of them are Прикладне програмне забезпечення 32 known as physiological regulators reacting to a drop in pressure in the reflexogenic zones of the arterial tree. Other regulators can be large- ly activated by the mechanical stretching of body structures. Therefore, the proper model must describe the effects of both mechanisms. Finally, the specific dynamics of blood pres- sure are associated with movements and re- distribution of significant volumes of blood under the influence of increased hydrostatic pressure. The quantitative mathematical model of human hemodynamics is the single method that can illustrate the cause-and-effect rela- tionships of developing dynamic events. It should be emphasized that the maximum ad- ditive effect of protective agents can only occur when each additional protective agent is activated at the right time. It can be detected using the mathematical model we create. To increase the visibility of the protec- tive effect, a special simulation mode will be provided when the physiological regulators are turned off. This simulation will reveal what could happen to hemodynamics if the body is late to respond to the mechanical movements of blood in the human body. In Fig. 1, the second group of models collects models quantitatively describing the influences of external mechanical dynamic forces on local, regional, or total hemodynam- ics. Namely, these models describe hemody- namic modulations of each protective tool and algorithm. In the right part of the Fig. 1, two addi- tional options are indicated. The bottom- located rectangle accentuates the fact that a special model will be proposed for the simula- tion of acceleration profiles. At last, the upper rectangle indicates that special logic and mathematic approximations must be proposed to individualize the physiology model using anthropometrics and the sex of the person to be tested (simulated). At last, the software must provide a computer experiment (simulation) and record- ing of its results as a special experiment pro- tocol (SEP). Personalized records of SEPs can be accumulated in special files for their re- producing and deep analysis. The latter must provide an option for comparing of chosen variables for at least two experiments. These basic requirements mainly determine the software architecture. The future software is intended to be autonomous Windows oriented. Exe module called “Accel.exe”. The success of software depends on two main factors: 1) how much it is needed; and 2) how practical is its user in- terface (UI). In our particular case, UI must be oriented both to student pilots and their train- ers-instructors. Therefore, icons intuitively appointing procedures needed to be activated for the program’s preparation before execut- ing is desirable. In addition, special icons in- tuitively appointing procedures for visualizing and analysis of simulation results are encour- aged. Fig.2 below indicates the main proce- dures necessary for preparing and executing a single computer experiment (simulation), and that have to be provided by a UI. Fig.2. Procedures that are necessary for pre- paring and executing a single computer exper- iment (simulation), and that have to be pro- vided by a special user interface (UI). 2. Main functional blocks of UI By downloading the future autonomous “Accel.exe”, the user will have a core (basic version) of the quantitative model that has to be specially tuned for providing a single com- puter experiment (simulation). The tuning operations, provided by the UI, are intended to transform the basic version of complex models to a person-oriented model possessing a set of constants characterizing both physio- logical and environmental parameters. Personal sensitivity of nervous regula- tors can vary in a wide range. There is no strain recommendation for associating the sensitivity coefficients with anthropometric data. At the same time, it is known that some tests (in particular, the postural test) can help Прикладне програмне забезпечення 33 us to approximately individualize the heart rate’s neurogenic sensitivity. During the pro- ject execution, several ideas have to be algo- rithmically realized and tested. Mathematical models The principle is to differentiate two blocks of mathematical models. The first block describes human hemodynamics under varying hydrostatic pressures and extravascu- lar pressures. The model does take into ac- count the main effects of physiological con- trol mechanisms that normally provide acute cardiovascular responses to dynamic accelera- tions. 1. The background of the physiological models The human cardiovascular system (CVS) must be presented in the model as a structure combined with two subunits. The first subunit represents the vascular bed as a net of arterial and venous compartments each localized at different distances from the foot level. Every vascular compartment will have its fixed initial parameters (rigidity )0(iD , unstressed volume )0(iU , and resistance )0(ir ). Current (dynamic) values of these variables will be calculated taking into ac- count increments provided by nervous- endocrine regulators: ,)0()( = j jii UUtU (1) ,)0()( = j jii DDtD (2) ))(),(()0()( tUtDrtr iiii = . (3) The principal is to model the influ- ences of gravitational and extravascular me- chanical forces on local output blood flows )(tqi : )(/))]()()(( ))()()([()( 111 trtPtPtP tPtPtPtq i E i G ii E i G iii +++ ++ −++= , (4) where the gravitational component )(tPG i is calculated using the distance of the vascular compartment from the foot ih , the current value of acceleration )(tGz , and the angle )(ti between acceleration vector and body vascular compartment. )(sin)()( ttGhtP izi G i  = . (4.1) As observation intervals under simu- lating of acceleration events are limited by minutes, the total blood volume .constV = Shifts of compartmental ( )(tVi ) and regional blood volumes appear due to alterations of compartmental input-output flows: ).()( 1 tqtq dt dV ii i −= − (5) Arterial baroreceptor reflexes are con- sidered to be the main physiological mecha- nisms counteracting to lowering of perfusion pressure in the brain [67]. In a rigid cranium, the normal extravascular pressure is slightly subatmospheric. +Gz accelerations, especially in non-collapsible venous sinuses, aggravate the negative pressure. These biomechanical factors, lowering the venous return from a cra- nial basin to the heart, play a specific counter- acting role against the gravitational decrease of brain circulation. Besides, within 50 mm Hg alterations of brain perfusion pressure, auto- nomic nervous mechanisms provide a practical constancy of the summary brain flow. Addi- tional protective effects are provided by a re- flector mechanism activated due to the lower- ing of intravascular pressure in the circle of Willis. This effect was first shown in [78]. Practically always real military fighter missions are accompanied by mental stress and delivery of catecholamines that addition- ally mobilize CVS. Empiric observations have also shown a phenomenon of heart rate extreme increase despite essentially elevated blood pressure in the aortic arch. This phe- nomenon can be explained and modeled in the assumption that under high levels of accelera- tion, the mechanical stress of muscles origi- nates high proprioception capable of compen- sating the depressor influence of the aortic arch baroreflex. 2. The background of models describing the physical environment Fighter pilots, functioning in a highly dynamic environment, are provided by artifi- cial specifically acting biomechanical protec- Прикладне програмне забезпечення 34 tive tools and methods. Standardly, they in- clude: i) a pilot’s chair with a declined to horizon under angle A supine; ii) anti-G suit; iii) a helmet provided by a device for breath- ing under positive pressure. To this list can be added special technics for tensing the muscles of the legs and abdominals. So, to simulate the protective effects of the artificial tools, additional equations describing the transformation of external bio- mechanical forces into the body’s regional vasculature are required. Simulation algo- rithms must provide applications of a chosen acceleration profile for every combination of protections. To demonstrate protection ef- fects, as well as to compare the effects of eve- ry single method, it desirable is to have two special model versions. The first one illus- trates hemodynamics under accelerations with switched-of physiological regulators. The second version does simulate hemodynamic responses of a person with the normal func- tioning of the physiological controllers of CVS. There are three specific ways to coun- teract extreme increases in vascular volume: 1) increasing the vascular rigidity; 2) decreas- ing the non-stressed volume; 3) elevating the extravascular pressure. The first two ways are incorporated into physiological reflector regulators. The third opportunity can be used without or with the application of artificial devices. In the first case, the person being under acceleration forces can consciously increase the tension in the muscles of the legs and abdominals. When additional efforts to exhale with a closed air- way have been provided, the protective effect is higher. Constructively, anti-G suits can be with pneumatic or water-filled chambers. The standard anti-G suit is sectional (for body sections of the abdomen, thighs, and shins). Versions of suits containing special sections for creating certain supra-atmospheric pres- sure at the chest are also proposed [6]. In gen- eral, these suits do resist the accumulation of local blood volumes. So, in the background of +Gz, a pumping of pressured air into the anti- G suit lowers the sectional blood volume. The matter is how to model these protective ef- fects. In equation (4) above, there is a varia- ble )(tPE i which presents local extravascular pressure. Certainly, leg muscles, abdomen, or thoracic cavities will have their transfer coef- ficients for transmitting the applied external pressure ( )(tPE ) to the depth of blood vessels. In (4), summary extravascular pressure should be calculated as: )()( tPktP Ei E i = . (4.2) 3. Models describing input loads The model to be used in the future software will calculate human hemodynamic responses to two different types of input dy- namic loads. During simulations of the pilot who is not using protections, the dynamics of accelerations are the lonely input loads initiat- ing alterations of the normal physiology of circulation and causing reflector responses. Protection activation should be considered as the second type of input load. Real flight ma- neuvers, especially combat maneuvers, occur under combined input loads. To estimate the separate effects of each input load, it is neces- sary to design algorithms providing arbitrary combinations of both types of input loads. Below, supposing the value of A to be con- stant, the first and the second types of input loads are consequentially considered. The initial hemodynamic alterations depend on both acceleration gradients and amplitude. So, to correctly simulate these biomechanical events, our software must include a model, describing accelerations dynamics. It is planned to provide the following acceleration profiles: a) a linear with a given gradient a and of  duration; b) a linear with a further transforming to a constant (plateau) of  du- ration; c) a trapezoidal with given parameters; d) a special profile for imitating the known “push-pull” effect; e) arbitrary constructing by a user profile. Formalisms for modeling these profiles are described below. The first profile is presented as:    −  = ssg s ttttA tt ta ),( ,0 )( , (6) where st - is start time of the increasing of acceleration with a gradient of gA . Прикладне програмне забезпечення 35 The second profile is presented as:      + −  = Tttta tttttA tt ta ppm pssg s , ),( ,0 )( , (7) where pt - is the time of reaching a plat- eau level with acceleration value of ma . The trapezoidal profile formalism looks as:        +−−− + −  = TttTttda Tttta ttttta att ta ppgm ppm pssg ms ),( , ),( 0;,0 )( , (8) where gd - is the deceleration gradient, T - is the plateau’s duration. Formalisms describing the second type of the input loads look as:      −   = mgmj mj atatda ataata ta tp )(0),( )(),( 0)(,0 )( 1 ,(9) where j can be altered step-like. Equations (1)-(9) were involved in this publication to help readers to understand our approach to the modeling. Much detailed in- formation one can find in [18-21]. The final version of the mathematical model describing the formal basis of the future software and simulation results will be published separately. Requirements to input and output data organization As already mentioned above, the “Ac- cel.exe” is planned to be autonomic software that provides an option for personalization. To satisfy these requirements, special algorithms are needed. They should provide initial data for characteristics of every vascular compart- ment, as well as for physiological regulators. In fact, this is the basic version of physiologi- cal models (BVPM). All additional proce- dures for BVPM’s personalizing using the input data must be algorithmically organized. 1. The input data BVPM should be tuned for the hemo- dynamics of a healthy man with mean anthro- pometric parameters of mas ( M ) and, height ( H ). Special formulas used M to calculate the total blood volume (V ) must be provided. Then, utilizing incorporated special massive of coefficients must be distributed in four cardiac chambers and 33 vascular (arterial and venous) compartments. Coefficients will characterize human horizontal position sec- tional or regional blood volumes. The next procedure does provide automatic recalculat- ing of these initial blood volumes to new ones characteristic for the relaxed human in a standard sitting position on a pilot armchair. Equations for these recalculations must take into account the initial parameterV . Individu- al anatomical peculiarities (if they are) con- cerning lengths of neck, tights, and shins have to be taken into account. 2. The output data There are planned two types of output data: one by default, and another – in special cases. The default data concerning accelera- tion profile, arterial pressures in three body zones (brain, eyes, aortic arch), and HR should have been presented in graph forms. This form is recommended to both student- pilots and instructors. Additional data includ- ing inside information about parameters of models is best to collect in table forms. Ex- perts developing advanced protections can be the users of these data. Namely, this class of users can prepare and simulate novel combat maneuvers avoiding risks for testers. Conclusion Combat maneuvers of modern fighter aircraft originate extreme accelerations nega- tively influencing on pilot’s physiology and operability. Empirical investigations were the only way to develop and test protective meth- ods and tools providing fighter pilots func- tionality under combat maneuvers. The main tools used for acquiring student pilot initial skills necessary to resist the negative effects of dynamic extreme accelerations were centri- Прикладне програмне забезпечення 36 fuges. The skilling process of student pilots of modern fighter aircraft is not duly formalized yet. Potentially, special computer simulators providing additional data concerning charac- teristics of both human physiology and pro- tective methods under dynamic accelerations could improve the skilling process and its efficiency. Certain scientific-practical prob- lems associated with creating the needed sim- ulator have been considered in the paper. To create special software, quantitative mathe- matical models must be previously created. 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Received: 05.02.2024 About authors: Grygoryan Rafik, Department chief, PhD, D-r in biology Publications number in Ukraine journals -124 Publications number in English journals -39. Hirsch index – 11 http://orcid.org/0000-0001-8762-733X Place of work: Institute of software systems of Ukraine National Academy of Sciences 03187, Кyїv, Acad. Glushkov avenue, 40, Е-mail:rgrygoryan@gmail.com .