TY  - JOUR
AU  - Dančuo, Zorana
AU  - Rašuo, Boško
AU  - Bengin, Aleksandar
AU  - Željković, Vladimir
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2836
AB  - Ovo istraživanje ima za cilj da doprinese slanju prve ljudske posade na Mars. U radu je simulirana anvelopa leta na Marsa u centrifugi visokih performansi. Visoka G-opterećenja prilikom poletanja, iskustvo nulte i mikrogravitacije, može rezultirati mnogim psiho-fiziološkim poremećajima kod astronauta. Ovo uslovljava potrebu za posebnim protokolima obuke. Predložena je anvelopa leta za prvu ljudsku misiju na Mars i simulirana u funkciji G-opterećenja. U radu su predloženi profili obuke. Poseban akcenat je stavljen na fazu lansiranja sa zemlje, kao i na fazu ponovnog ulaska i sletanja. Ponovni ulazak može biti posebno opasan, uz mnogo veća ubrzanja. Precizna simulacija zahteva pravilno podešavanje rotacionih uglova centrifuge. Prilagođavanje uglova se vrši u cilju smanjenja bočnih i poprečnih G-opterećenja. Ova studija će, nadamo se, pomoći da se čovečanstvo približi snu “Ljudi na Marsu”.
AB  - This research is an effort to contribute to the human exploration of Mars by simulating phases of the Mars flight envelope in a high performance human centrifuge. The crushing sensation experienced at high-G levels during take-off, the experience of zero and microgravity, can result in many psycho-problems to astronauts, obviating the need for realistic training protocols. The flight envelope for the first manned mission to Mars is proposed, and simulated in terms of G- load. Some training profile suggestions are given. A special emphasis is placed on the Earth launch phase, and on the Earth re-entry and landing phase. Re-entry can be especially dangerous with much higher accelerations. Accurate simulation requires a proper adjustment of rotational angles of the centrifuge. Angle adjustments are made in order to minimize side-Gy and transverse-Gx load. This study will hopefully help to move faster towards the dream of “Humans on Mars”.
PB  - Univerzitet u Beogradu - Mašinski fakultet, Beograd
T2  - FME Transactions
T1  - Let na Mars - simulacija anvelope u centrifugi visokih performansi na zemlji
T1  - Flight to Mars: Envelope simulation in a ground based high-performance human centrifuge
EP  - 9
IS  - 1
SP  - 1
VL  - 46
DO  - 10.5937/fmet1801001D
ER  - 

@article{
author = "Dančuo, Zorana and Rašuo, Boško and Bengin, Aleksandar and Željković, Vladimir",
year = "2018",
abstract = "Ovo istraživanje ima za cilj da doprinese slanju prve ljudske posade na Mars. U radu je simulirana anvelopa leta na Marsa u centrifugi visokih performansi. Visoka G-opterećenja prilikom poletanja, iskustvo nulte i mikrogravitacije, može rezultirati mnogim psiho-fiziološkim poremećajima kod astronauta. Ovo uslovljava potrebu za posebnim protokolima obuke. Predložena je anvelopa leta za prvu ljudsku misiju na Mars i simulirana u funkciji G-opterećenja. U radu su predloženi profili obuke. Poseban akcenat je stavljen na fazu lansiranja sa zemlje, kao i na fazu ponovnog ulaska i sletanja. Ponovni ulazak može biti posebno opasan, uz mnogo veća ubrzanja. Precizna simulacija zahteva pravilno podešavanje rotacionih uglova centrifuge. Prilagođavanje uglova se vrši u cilju smanjenja bočnih i poprečnih G-opterećenja. Ova studija će, nadamo se, pomoći da se čovečanstvo približi snu “Ljudi na Marsu”., This research is an effort to contribute to the human exploration of Mars by simulating phases of the Mars flight envelope in a high performance human centrifuge. The crushing sensation experienced at high-G levels during take-off, the experience of zero and microgravity, can result in many psycho-problems to astronauts, obviating the need for realistic training protocols. The flight envelope for the first manned mission to Mars is proposed, and simulated in terms of G- load. Some training profile suggestions are given. A special emphasis is placed on the Earth launch phase, and on the Earth re-entry and landing phase. Re-entry can be especially dangerous with much higher accelerations. Accurate simulation requires a proper adjustment of rotational angles of the centrifuge. Angle adjustments are made in order to minimize side-Gy and transverse-Gx load. This study will hopefully help to move faster towards the dream of “Humans on Mars”.",
publisher = "Univerzitet u Beogradu - Mašinski fakultet, Beograd",
journal = "FME Transactions",
title = "Let na Mars - simulacija anvelope u centrifugi visokih performansi na zemlji, Flight to Mars: Envelope simulation in a ground based high-performance human centrifuge",
pages = "9-1",
number = "1",
volume = "46",
doi = "10.5937/fmet1801001D"
}

Dančuo, Z., Rašuo, B., Bengin, A.,& Željković, V.. (2018). Let na Mars - simulacija anvelope u centrifugi visokih performansi na zemlji. in FME Transactions
Univerzitet u Beogradu - Mašinski fakultet, Beograd., 46(1), 1-9.
https://doi.org/10.5937/fmet1801001D

Dančuo Z, Rašuo B, Bengin A, Željković V. Let na Mars - simulacija anvelope u centrifugi visokih performansi na zemlji. in FME Transactions. 2018;46(1):1-9.
doi:10.5937/fmet1801001D .

Dančuo, Zorana, Rašuo, Boško, Bengin, Aleksandar, Željković, Vladimir, "Let na Mars - simulacija anvelope u centrifugi visokih performansi na zemlji" in FME Transactions, 46, no. 1 (2018):1-9,
https://doi.org/10.5937/fmet1801001D . .

TY  - CONF
AU  - Dančuo, Zorana
AU  - Rašuo, Boško
AU  - Željković, Vladimir
PY  - 2013
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/1758
AB  - This paper represents an effort to enhance and contribute to the human exploration of Mars, by simulating phases of the Earth-Mars-Earth flight envelope in a high performance human centrifuge. Humans are the most valuable part of the Mars mission. The crew will encounter the Space, interplanetary and planetary surface environment, and has to remain productive during the whole mission. The crushing sensation experienced at high-G levels during take-off, zero and microgravity, can cause many psycho-physiological problems to astronauts. The human body undergoes major changes in Space, especially when returning from weightlessness and readapting to gravity. The centrifuge discussed in this paper, is in essence a robotic manipulator with three degrees of freedom of motion. It is capable of achieving extreme G-loads in short time intervals. In order to achieve an extreme gradient, the main drive of the centrifuge has to work with an overload in a short time interval. This allows an authentic G-simulation. The centrifuge has an onset rate of 9G/s. It consists of three independent controllable axes (angles): the roll, pitch and the planetary axis. The flight envelope for the possible manned Mars mission is examined, and simulated in terms of G in this paper. In order to get better acquainted with the conditions astronauts will be exposed in flight, and to improve astronaut training for the Mars mission, some training profile suggestions are also given in this paper. A special emphasis is placed on the Earth launch phase, as well as on the Earth entry and landing phase. The experience of launch, ascent, re-entry is simulated in terms of G. Astronauts experience a load of about 3G during take-off. Reentry can be especially dangerous with much higher accelerations, beside the fact that astronauts wear anti-G suits. Simulating the Earth-Mars-Earth envelope accurately requires a proper adjustment of the three rotational angles, which is also given in this study. The longitudinal G-load is most important for training, given that it has the highest value in real flight. Angle adjustments are made in order to minimize side-load and transverse load, although the centrifuge may provide all three loads. The Earth-Mars-Earth envelope consists of many critical phases. Envelope simulations in a centrifuge are valuable for astronauts. Flight simulation is an essential component of aircrew training, providing a safe and reliable training environment. This will hopefully help to move faster towards the dream called "Humans on Mars".
PB  - International Astronautical Federation, IAF
C3  - Proceedings of the International Astronautical Congress, IAC
T1  - Mars evelope simulation in a high-performance human centrifuge
EP  - 1800
SP  - 1791
VL  - 3
UR  - https://hdl.handle.net/21.15107/rcub_machinery_1758
ER  - 

@conference{
author = "Dančuo, Zorana and Rašuo, Boško and Željković, Vladimir",
year = "2013",
abstract = "This paper represents an effort to enhance and contribute to the human exploration of Mars, by simulating phases of the Earth-Mars-Earth flight envelope in a high performance human centrifuge. Humans are the most valuable part of the Mars mission. The crew will encounter the Space, interplanetary and planetary surface environment, and has to remain productive during the whole mission. The crushing sensation experienced at high-G levels during take-off, zero and microgravity, can cause many psycho-physiological problems to astronauts. The human body undergoes major changes in Space, especially when returning from weightlessness and readapting to gravity. The centrifuge discussed in this paper, is in essence a robotic manipulator with three degrees of freedom of motion. It is capable of achieving extreme G-loads in short time intervals. In order to achieve an extreme gradient, the main drive of the centrifuge has to work with an overload in a short time interval. This allows an authentic G-simulation. The centrifuge has an onset rate of 9G/s. It consists of three independent controllable axes (angles): the roll, pitch and the planetary axis. The flight envelope for the possible manned Mars mission is examined, and simulated in terms of G in this paper. In order to get better acquainted with the conditions astronauts will be exposed in flight, and to improve astronaut training for the Mars mission, some training profile suggestions are also given in this paper. A special emphasis is placed on the Earth launch phase, as well as on the Earth entry and landing phase. The experience of launch, ascent, re-entry is simulated in terms of G. Astronauts experience a load of about 3G during take-off. Reentry can be especially dangerous with much higher accelerations, beside the fact that astronauts wear anti-G suits. Simulating the Earth-Mars-Earth envelope accurately requires a proper adjustment of the three rotational angles, which is also given in this study. The longitudinal G-load is most important for training, given that it has the highest value in real flight. Angle adjustments are made in order to minimize side-load and transverse load, although the centrifuge may provide all three loads. The Earth-Mars-Earth envelope consists of many critical phases. Envelope simulations in a centrifuge are valuable for astronauts. Flight simulation is an essential component of aircrew training, providing a safe and reliable training environment. This will hopefully help to move faster towards the dream called "Humans on Mars".",
publisher = "International Astronautical Federation, IAF",
journal = "Proceedings of the International Astronautical Congress, IAC",
title = "Mars evelope simulation in a high-performance human centrifuge",
pages = "1800-1791",
volume = "3",
url = "https://hdl.handle.net/21.15107/rcub_machinery_1758"
}

Dančuo, Z., Rašuo, B.,& Željković, V.. (2013). Mars evelope simulation in a high-performance human centrifuge. in Proceedings of the International Astronautical Congress, IAC
International Astronautical Federation, IAF., 3, 1791-1800.
https://hdl.handle.net/21.15107/rcub_machinery_1758

Dančuo Z, Rašuo B, Željković V. Mars evelope simulation in a high-performance human centrifuge. in Proceedings of the International Astronautical Congress, IAC. 2013;3:1791-1800.
https://hdl.handle.net/21.15107/rcub_machinery_1758 .

Dančuo, Zorana, Rašuo, Boško, Željković, Vladimir, "Mars evelope simulation in a high-performance human centrifuge" in Proceedings of the International Astronautical Congress, IAC, 3 (2013):1791-1800,
https://hdl.handle.net/21.15107/rcub_machinery_1758 .

TY  - JOUR
AU  - Dančuo, Zorana
AU  - Rašuo, Boško
AU  - Željković, Vladimir
AU  - Đapić, Mirko
PY  - 2012
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/1362
AB  - Razvoj humane centrifuge visokih performansi ima za cilj da izađe u susret zahtevima za stvaranje sigurnog i bezbednog okruženja za trening pilota borbenih aviona, radi ispitivanja njihove tolerancije na velika opterećenja. Svrha razvoja uređaja za obuku, je da se ustanovi kako nespecifični režimi leta deluju na individualnu fiziologiju pilota na obuci, kao i njegovu sposobnost optimalnog izvođenja borbene misije pod datim opterećenjem. Razvoj je baziran na rešavanju strukturalnih problema, kreiranju kinematskih, dinamičkih i kontrolnih algoritama za simulaciju. Humana centrifuga, izložena u ovom radu, je projektovana kao sistem sa tri stepena slobode kretanja. Zbog izuzetnih performansi, uređaj centrifuge nalazi značajnu primenu u testiranju izdržljivosti materijala i avionske opreme. Na Institutu Lola, biće razvijen model u odgovarajućoj razmeri. Cilj razvoja centrifuge visokih performansi je, pre svega, da se simuliraju specifična opterećenja supermanevara i time obezbedi optimalan trenažni režim pilota, izlažući pilota na obuci velikom priraštaju opterećenja u kratkom vremenskom intervalu.
AB  - In this paper some aspects of Human Centrifuge development are given. The main objective is to emphasize the importance of high G pilots training. Terms such as 'high agility' and 'supermaeuverability' are briefly explained. The development of a High Performance Centrifuge is intended to meet requirements for creating a safe and secure environment for fighter pilots training. The purpose is to determine how non-specific flight regimes affect the individual physiology, as well as the ability to perform combat missions under a given load. The development is based on structural problems, creation of kinematic, dynamic and control algorithms. The Human Centrifuge, presented in this paper is designed as a system of three Degrees of Freedom of Motion. Due to its exceptional performances, the device has an important application in material testing and sustainability of overall airborne equipment. The manipulator will be produced in an appropriate ratio, as a model. The main goal of this paper is to underline the importance of optimal training, by ensuring a high G onset rate. Also, some basic technical data and diagrams are given, in order to make the reader familiar to motion simulation basics.
PB  - Savez inženjera i tehničara Srbije, Beograd
T2  - Tehnika
T1  - Osnovi razvoja humane centrifuge visokih performansi
T1  - Basics of high performance human centrifuge development
EP  - 577
IS  - 4
SP  - 573
VL  - 67
UR  - https://hdl.handle.net/21.15107/rcub_machinery_1362
ER  - 

@article{
author = "Dančuo, Zorana and Rašuo, Boško and Željković, Vladimir and Đapić, Mirko",
year = "2012",
abstract = "Razvoj humane centrifuge visokih performansi ima za cilj da izađe u susret zahtevima za stvaranje sigurnog i bezbednog okruženja za trening pilota borbenih aviona, radi ispitivanja njihove tolerancije na velika opterećenja. Svrha razvoja uređaja za obuku, je da se ustanovi kako nespecifični režimi leta deluju na individualnu fiziologiju pilota na obuci, kao i njegovu sposobnost optimalnog izvođenja borbene misije pod datim opterećenjem. Razvoj je baziran na rešavanju strukturalnih problema, kreiranju kinematskih, dinamičkih i kontrolnih algoritama za simulaciju. Humana centrifuga, izložena u ovom radu, je projektovana kao sistem sa tri stepena slobode kretanja. Zbog izuzetnih performansi, uređaj centrifuge nalazi značajnu primenu u testiranju izdržljivosti materijala i avionske opreme. Na Institutu Lola, biće razvijen model u odgovarajućoj razmeri. Cilj razvoja centrifuge visokih performansi je, pre svega, da se simuliraju specifična opterećenja supermanevara i time obezbedi optimalan trenažni režim pilota, izlažući pilota na obuci velikom priraštaju opterećenja u kratkom vremenskom intervalu., In this paper some aspects of Human Centrifuge development are given. The main objective is to emphasize the importance of high G pilots training. Terms such as 'high agility' and 'supermaeuverability' are briefly explained. The development of a High Performance Centrifuge is intended to meet requirements for creating a safe and secure environment for fighter pilots training. The purpose is to determine how non-specific flight regimes affect the individual physiology, as well as the ability to perform combat missions under a given load. The development is based on structural problems, creation of kinematic, dynamic and control algorithms. The Human Centrifuge, presented in this paper is designed as a system of three Degrees of Freedom of Motion. Due to its exceptional performances, the device has an important application in material testing and sustainability of overall airborne equipment. The manipulator will be produced in an appropriate ratio, as a model. The main goal of this paper is to underline the importance of optimal training, by ensuring a high G onset rate. Also, some basic technical data and diagrams are given, in order to make the reader familiar to motion simulation basics.",
publisher = "Savez inženjera i tehničara Srbije, Beograd",
journal = "Tehnika",
title = "Osnovi razvoja humane centrifuge visokih performansi, Basics of high performance human centrifuge development",
pages = "577-573",
number = "4",
volume = "67",
url = "https://hdl.handle.net/21.15107/rcub_machinery_1362"
}

Dančuo, Z., Rašuo, B., Željković, V.,& Đapić, M.. (2012). Osnovi razvoja humane centrifuge visokih performansi. in Tehnika
Savez inženjera i tehničara Srbije, Beograd., 67(4), 573-577.
https://hdl.handle.net/21.15107/rcub_machinery_1362

Dančuo Z, Rašuo B, Željković V, Đapić M. Osnovi razvoja humane centrifuge visokih performansi. in Tehnika. 2012;67(4):573-577.
https://hdl.handle.net/21.15107/rcub_machinery_1362 .

Dančuo, Zorana, Rašuo, Boško, Željković, Vladimir, Đapić, Mirko, "Osnovi razvoja humane centrifuge visokih performansi" in Tehnika, 67, no. 4 (2012):573-577,
https://hdl.handle.net/21.15107/rcub_machinery_1362 .

TY  - JOUR
AU  - Dančuo, Zorana
AU  - Rašuo, Boško
AU  - Kvrgić, Vladimir
AU  - Željković, Vladimir
PY  - 2012
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/1473
AB  - U ovom radu je iznet je problem izbora glavnog pogona za humanu centrifugu, počev od anvelope leta koju je potrebno simulirati. Osnovni cilj je da se naglasi složenost izbora pogona, jer je u pitanju motor velike snage. Metodologija izbora glavnog pogona centrifuge za obuku pilota, koja predstavlja manipulator sa tri stepena slobode kretanja, zasnovana je na glavnom zahtevu, da se postigne ekstremni gradijent i koeficijent opterećenja u jedinici vremena. Metodologija se sastoji u određivanju potrebnog obrtnog momenta i snage glavnog pogona centrifuge. Da bi se postigao osnovni zahtev, motor mora raditi sa preopterećenjem u datom vremenskom intervalu u početnom trenutku. Za proračune i dijagrame, program MATLAB je korišćen. U ovom radu dat je primer motora švajcarskog proizvođača ABB. Njegove karakteristike su objašnjene detaljno, u odnosu na potrebni obrtni moment i snagu glavnog pogona. Sve numeričke vrednosti u ovom radu, su deo preliminarnog proračuna.
AB  - In this paper, the issue of the main drive selection for a Human Centrifuge is explained, starting from the flight envelope that needs to be simulated. The main objective is to emphasize the complexity of choosing a drive, since it is a high power drive. The methodology for the main drive selection of a Centrifuge for pilot training, which is a manipulator with three degrees of freedom of motion, is built upon the main demand to achieve an extreme gradient and load coefficient per unit of time. The methodology consists of determining the necessary torque and power of the main drive of the Centrifuge. To achieve the main requirement, the engine has to work with an overload in a given time interval at the beginning. For calculations and diagrams, the MATLAB program was used. In this paper, an example of a motor of the Swiss manufacturer ABB is given. Its features are explained in detail, according to the needed torque and power of the main drive. All numerical values in this paper, are a part of a preliminary calculation.
PB  - Univerzitet u Beogradu - Mašinski fakultet, Beograd
T2  - FME Transactions
T1  - Metodologija izbora glavnog pogona za humanu centrifugu
T1  - Methodology of the main drive selection for a human centrifuge
EP  - 74
IS  - 2
SP  - 69
VL  - 40
UR  - https://hdl.handle.net/21.15107/rcub_machinery_1473
ER  - 

@article{
author = "Dančuo, Zorana and Rašuo, Boško and Kvrgić, Vladimir and Željković, Vladimir",
year = "2012",
abstract = "U ovom radu je iznet je problem izbora glavnog pogona za humanu centrifugu, počev od anvelope leta koju je potrebno simulirati. Osnovni cilj je da se naglasi složenost izbora pogona, jer je u pitanju motor velike snage. Metodologija izbora glavnog pogona centrifuge za obuku pilota, koja predstavlja manipulator sa tri stepena slobode kretanja, zasnovana je na glavnom zahtevu, da se postigne ekstremni gradijent i koeficijent opterećenja u jedinici vremena. Metodologija se sastoji u određivanju potrebnog obrtnog momenta i snage glavnog pogona centrifuge. Da bi se postigao osnovni zahtev, motor mora raditi sa preopterećenjem u datom vremenskom intervalu u početnom trenutku. Za proračune i dijagrame, program MATLAB je korišćen. U ovom radu dat je primer motora švajcarskog proizvođača ABB. Njegove karakteristike su objašnjene detaljno, u odnosu na potrebni obrtni moment i snagu glavnog pogona. Sve numeričke vrednosti u ovom radu, su deo preliminarnog proračuna., In this paper, the issue of the main drive selection for a Human Centrifuge is explained, starting from the flight envelope that needs to be simulated. The main objective is to emphasize the complexity of choosing a drive, since it is a high power drive. The methodology for the main drive selection of a Centrifuge for pilot training, which is a manipulator with three degrees of freedom of motion, is built upon the main demand to achieve an extreme gradient and load coefficient per unit of time. The methodology consists of determining the necessary torque and power of the main drive of the Centrifuge. To achieve the main requirement, the engine has to work with an overload in a given time interval at the beginning. For calculations and diagrams, the MATLAB program was used. In this paper, an example of a motor of the Swiss manufacturer ABB is given. Its features are explained in detail, according to the needed torque and power of the main drive. All numerical values in this paper, are a part of a preliminary calculation.",
publisher = "Univerzitet u Beogradu - Mašinski fakultet, Beograd",
journal = "FME Transactions",
title = "Metodologija izbora glavnog pogona za humanu centrifugu, Methodology of the main drive selection for a human centrifuge",
pages = "74-69",
number = "2",
volume = "40",
url = "https://hdl.handle.net/21.15107/rcub_machinery_1473"
}

Dančuo, Z., Rašuo, B., Kvrgić, V.,& Željković, V.. (2012). Metodologija izbora glavnog pogona za humanu centrifugu. in FME Transactions
Univerzitet u Beogradu - Mašinski fakultet, Beograd., 40(2), 69-74.
https://hdl.handle.net/21.15107/rcub_machinery_1473

Dančuo Z, Rašuo B, Kvrgić V, Željković V. Metodologija izbora glavnog pogona za humanu centrifugu. in FME Transactions. 2012;40(2):69-74.
https://hdl.handle.net/21.15107/rcub_machinery_1473 .

Dančuo, Zorana, Rašuo, Boško, Kvrgić, Vladimir, Željković, Vladimir, "Metodologija izbora glavnog pogona za humanu centrifugu" in FME Transactions, 40, no. 2 (2012):69-74,
https://hdl.handle.net/21.15107/rcub_machinery_1473 .

TY  - JOUR
AU  - Dančuo, Zorana
AU  - Željković, Vladimir
AU  - Rašuo, Boško
AU  - Đapić, Mirko
PY  - 2012
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/1422
AB  - U ovom radu predstavljeni su profili za obuku u humanoj centrifugi visokih performansi. Glavni cilj je da se istakne značaj razvoja različitih trening scenarija, kako bi se postigla optimalna spremnost pilota borbenih aviona. Ovo istraživanje bazirano je na standardu NATO STANAG 3827 AMD-a, koji propisuje vrednosti G tolerancija, koju posada treba da podnese. Posada koja ne završi uspešno trening Rapid Onset Rate (ROR) 7G za 15 sekundi sa anti-G odelom i Anti-G Straining maneuver-om (AGSM), smatraće se da ima nizak prag tolerancije na G opterećenje, što je objašnjeno detaljno u ovom radu. Profili za obuku su grafički predstavljeni, kao i ugaona brzina kraka, ugao valjanja i ugao propinjanja-poniranja za svaku vrednost opterećenja. Glavni zahtev humane centrifuge predstavljene u ovom radu, je da se postigne gradijent ubrzanja od 9G/s. Profili koji su prikazani u ovom radu su deo istraživanja Lola Instituta u Beogradu. U radu su dati i primeri scenarija za obuku pilota koji se primenjuju u nekoliko zemalja. G opterećenja koja prouzrokuju gubitak svesti kod pilota (G-LOC) su deo scenarija i neizbežna su tokom treninga u centrifugi. Efektivna obuka AGSM i povećanje G-tolerancija pilota, doprinose bezbednosti leta i na taj način se smanjuje rizik od G-LOC i vazduhoplovnih nesreća. Cilj ovog rada je da ilustruje značaj i složenost upravljanja i podešavanja parametara rada, kako bi se postiglo željeno opterećenje. .
AB  - In this paper, profiles for training in a High Performance Human Centrifuge (HPHC) are presented. The main objective is to underline the significance of developing various training scenarios in order to achieve optimal preparedness of fighter pilots. This research is based on the NATO STANAG 3827 AMD, a standard that provides values of G tolerance that an aircrew must sustain. An aircrew who do not successfully complete a Rapid Onset Rate (ROR) 7G for 15 seconds centrifuge profile with anti-G suit and straining maneuver will be considered to have low G tolerance, which is explained in detail in this paper. Training profiles are presented graphically, as well as arm angular velocity, roll and pitch angle for each load. The main demand for the Human Centrifuge presented in this paper is to achieve an onset rate of 9G/s. The graphs in this paper are a part of the research conducted in the Lola Institute Belgrade. The examples of training scenarios of several countries are given briefly. G-Induced Loss of Consciousness (G-LOC) episodes are unavoidable during centrifuge training. Effective training of Anti-G Straining Maneuver (AGSM) and increasing pilots G-tolerance contribute to flight safety and thereby reduce the risk of G-LOC and aircraft accidents. The aim of this paper is to illustrate the complexity of parameter settings in order to achieve desired loads. .
PB  - Vojnotehnički institut, Beograd
T2  - Scientific Technical Review
T1  - G profili za obuku u humanoj centrifugi visokih performansi
T1  - High G training profiles in a high performance human centrifuge
EP  - 69
IS  - 1
SP  - 64
VL  - 62
UR  - https://hdl.handle.net/21.15107/rcub_machinery_1422
ER  - 

@article{
author = "Dančuo, Zorana and Željković, Vladimir and Rašuo, Boško and Đapić, Mirko",
year = "2012",
abstract = "U ovom radu predstavljeni su profili za obuku u humanoj centrifugi visokih performansi. Glavni cilj je da se istakne značaj razvoja različitih trening scenarija, kako bi se postigla optimalna spremnost pilota borbenih aviona. Ovo istraživanje bazirano je na standardu NATO STANAG 3827 AMD-a, koji propisuje vrednosti G tolerancija, koju posada treba da podnese. Posada koja ne završi uspešno trening Rapid Onset Rate (ROR) 7G za 15 sekundi sa anti-G odelom i Anti-G Straining maneuver-om (AGSM), smatraće se da ima nizak prag tolerancije na G opterećenje, što je objašnjeno detaljno u ovom radu. Profili za obuku su grafički predstavljeni, kao i ugaona brzina kraka, ugao valjanja i ugao propinjanja-poniranja za svaku vrednost opterećenja. Glavni zahtev humane centrifuge predstavljene u ovom radu, je da se postigne gradijent ubrzanja od 9G/s. Profili koji su prikazani u ovom radu su deo istraživanja Lola Instituta u Beogradu. U radu su dati i primeri scenarija za obuku pilota koji se primenjuju u nekoliko zemalja. G opterećenja koja prouzrokuju gubitak svesti kod pilota (G-LOC) su deo scenarija i neizbežna su tokom treninga u centrifugi. Efektivna obuka AGSM i povećanje G-tolerancija pilota, doprinose bezbednosti leta i na taj način se smanjuje rizik od G-LOC i vazduhoplovnih nesreća. Cilj ovog rada je da ilustruje značaj i složenost upravljanja i podešavanja parametara rada, kako bi se postiglo željeno opterećenje. ., In this paper, profiles for training in a High Performance Human Centrifuge (HPHC) are presented. The main objective is to underline the significance of developing various training scenarios in order to achieve optimal preparedness of fighter pilots. This research is based on the NATO STANAG 3827 AMD, a standard that provides values of G tolerance that an aircrew must sustain. An aircrew who do not successfully complete a Rapid Onset Rate (ROR) 7G for 15 seconds centrifuge profile with anti-G suit and straining maneuver will be considered to have low G tolerance, which is explained in detail in this paper. Training profiles are presented graphically, as well as arm angular velocity, roll and pitch angle for each load. The main demand for the Human Centrifuge presented in this paper is to achieve an onset rate of 9G/s. The graphs in this paper are a part of the research conducted in the Lola Institute Belgrade. The examples of training scenarios of several countries are given briefly. G-Induced Loss of Consciousness (G-LOC) episodes are unavoidable during centrifuge training. Effective training of Anti-G Straining Maneuver (AGSM) and increasing pilots G-tolerance contribute to flight safety and thereby reduce the risk of G-LOC and aircraft accidents. The aim of this paper is to illustrate the complexity of parameter settings in order to achieve desired loads. .",
publisher = "Vojnotehnički institut, Beograd",
journal = "Scientific Technical Review",
title = "G profili za obuku u humanoj centrifugi visokih performansi, High G training profiles in a high performance human centrifuge",
pages = "69-64",
number = "1",
volume = "62",
url = "https://hdl.handle.net/21.15107/rcub_machinery_1422"
}

Dančuo, Z., Željković, V., Rašuo, B.,& Đapić, M.. (2012). G profili za obuku u humanoj centrifugi visokih performansi. in Scientific Technical Review
Vojnotehnički institut, Beograd., 62(1), 64-69.
https://hdl.handle.net/21.15107/rcub_machinery_1422

Dančuo Z, Željković V, Rašuo B, Đapić M. G profili za obuku u humanoj centrifugi visokih performansi. in Scientific Technical Review. 2012;62(1):64-69.
https://hdl.handle.net/21.15107/rcub_machinery_1422 .

Dančuo, Zorana, Željković, Vladimir, Rašuo, Boško, Đapić, Mirko, "G profili za obuku u humanoj centrifugi visokih performansi" in Scientific Technical Review, 62, no. 1 (2012):64-69,
https://hdl.handle.net/21.15107/rcub_machinery_1422 .

TY  - CONF
AU  - Dančuo, Zorana
AU  - Rańuo, B.
AU  - Željković, Vladimir
AU  - Vidaković, Jelena
AU  - Kvrgić, Vladimir
PY  - 2012
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/1553
PB  - University of Belgrade
C3  - 29th DANUBlA-ADRIA Symposium on Advances in Experimental Mechanics, DAS 2012
T1  - Accelerations in a high permance human centrifuge
EP  - 185
SP  - 182
UR  - https://hdl.handle.net/21.15107/rcub_machinery_1553
ER  - 

@conference{
author = "Dančuo, Zorana and Rańuo, B. and Željković, Vladimir and Vidaković, Jelena and Kvrgić, Vladimir",
year = "2012",
publisher = "University of Belgrade",
journal = "29th DANUBlA-ADRIA Symposium on Advances in Experimental Mechanics, DAS 2012",
title = "Accelerations in a high permance human centrifuge",
pages = "185-182",
url = "https://hdl.handle.net/21.15107/rcub_machinery_1553"
}

Dančuo, Z., Rańuo, B., Željković, V., Vidaković, J.,& Kvrgić, V.. (2012). Accelerations in a high permance human centrifuge. in 29th DANUBlA-ADRIA Symposium on Advances in Experimental Mechanics, DAS 2012
University of Belgrade., 182-185.
https://hdl.handle.net/21.15107/rcub_machinery_1553

Dančuo Z, Rańuo B, Željković V, Vidaković J, Kvrgić V. Accelerations in a high permance human centrifuge. in 29th DANUBlA-ADRIA Symposium on Advances in Experimental Mechanics, DAS 2012. 2012;:182-185.
https://hdl.handle.net/21.15107/rcub_machinery_1553 .

Dančuo, Zorana, Rańuo, B., Željković, Vladimir, Vidaković, Jelena, Kvrgić, Vladimir, "Accelerations in a high permance human centrifuge" in 29th DANUBlA-ADRIA Symposium on Advances in Experimental Mechanics, DAS 2012 (2012):182-185,
https://hdl.handle.net/21.15107/rcub_machinery_1553 .