CVETKOVIČ, Dragan ;RADAKOVIĆ, Duško . Mathematical Models of Helicopter Flight Dynamics. Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 53, n.2, p. 114-126, october 2017. ISSN 0039-2480. Available at: <https://www.sv-jme.eu/sl/article/mathematical-models-of-helicopter-flight-dynamics/>. Date accessed: 19 apr. 2024. doi:http://dx.doi.org/.
Cvetkovič, D., & Radaković, D. (2007). Mathematical Models of Helicopter Flight Dynamics. Strojniški vestnik - Journal of Mechanical Engineering, 53(2), 114-126. doi:http://dx.doi.org/
@article{.,
author = {Dragan Cvetkovič and Duško Radaković},
title = {Mathematical Models of Helicopter Flight Dynamics},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {53},
number = {2},
year = {2007},
keywords = {helicopters; flight dynamics; mathematical models; },
abstract = {The helicopter is a specific form of traffic-transportation, not just in terms of its structure but also in terms of its possibilities for motion. The helicopter can move vertically, hover in the air, turn around, move forward and move laterally, and it can also perform combinations of these movements. As a result, modeling and testing helicopter dynamics is a very complex problem. The problems in helicopter flight dynamics are mostly solved with the aid of modern computers. Though inevitably, with many complex problems, computers do not make it possible to understand the physical nature of the problem. Fortunately, many problems related to helicopters can be analyzed without overly complex calculus, and usually it is possible to obtain simple formulae. Though not suitable for calculus, these formulae, when designing the helicopter, enable a satisfactory interpretation of the required aerodynamic and dynamic phenomena. The helicopter belongs to the group of aerospace systems and its traditional modeling may be divided into: a) three-dimensional (space) geometry and kinematics, and b) rigid-body dynamics and the fluid dynamics through which it moves. Recently, the following models were developed: c) the elasticity model in intersubordinance with a fluid, d) the propulsion system model, e) the hydraulic model and other actuators that achieve aerodynamic control, f) the pilot-behavior model, g) the navigation-system model, and h) the beacon-problem model. The mathematical model described in this paper is related to a) and b).},
issn = {0039-2480}, pages = {114-126}, doi = {},
url = {https://www.sv-jme.eu/sl/article/mathematical-models-of-helicopter-flight-dynamics/}
}
Cvetkovič, D.,Radaković, D. 2007 October 53. Mathematical Models of Helicopter Flight Dynamics. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 53:2
%A Cvetkovič, Dragan %A Radaković, Duško %D 2007 %T Mathematical Models of Helicopter Flight Dynamics %B 2007 %9 helicopters; flight dynamics; mathematical models; %! Mathematical Models of Helicopter Flight Dynamics %K helicopters; flight dynamics; mathematical models; %X The helicopter is a specific form of traffic-transportation, not just in terms of its structure but also in terms of its possibilities for motion. The helicopter can move vertically, hover in the air, turn around, move forward and move laterally, and it can also perform combinations of these movements. As a result, modeling and testing helicopter dynamics is a very complex problem. The problems in helicopter flight dynamics are mostly solved with the aid of modern computers. Though inevitably, with many complex problems, computers do not make it possible to understand the physical nature of the problem. Fortunately, many problems related to helicopters can be analyzed without overly complex calculus, and usually it is possible to obtain simple formulae. Though not suitable for calculus, these formulae, when designing the helicopter, enable a satisfactory interpretation of the required aerodynamic and dynamic phenomena. The helicopter belongs to the group of aerospace systems and its traditional modeling may be divided into: a) three-dimensional (space) geometry and kinematics, and b) rigid-body dynamics and the fluid dynamics through which it moves. Recently, the following models were developed: c) the elasticity model in intersubordinance with a fluid, d) the propulsion system model, e) the hydraulic model and other actuators that achieve aerodynamic control, f) the pilot-behavior model, g) the navigation-system model, and h) the beacon-problem model. The mathematical model described in this paper is related to a) and b). %U https://www.sv-jme.eu/sl/article/mathematical-models-of-helicopter-flight-dynamics/ %0 Journal Article %R %& 114 %P 13 %J Strojniški vestnik - Journal of Mechanical Engineering %V 53 %N 2 %@ 0039-2480 %8 2017-10-24 %7 2017-10-24
Cvetkovič, Dragan, & Duško Radaković. "Mathematical Models of Helicopter Flight Dynamics." Strojniški vestnik - Journal of Mechanical Engineering [Online], 53.2 (2007): 114-126. Web. 19 Apr. 2024
TY - JOUR AU - Cvetkovič, Dragan AU - Radaković, Duško PY - 2007 TI - Mathematical Models of Helicopter Flight Dynamics JF - Strojniški vestnik - Journal of Mechanical Engineering DO - KW - helicopters; flight dynamics; mathematical models; N2 - The helicopter is a specific form of traffic-transportation, not just in terms of its structure but also in terms of its possibilities for motion. The helicopter can move vertically, hover in the air, turn around, move forward and move laterally, and it can also perform combinations of these movements. As a result, modeling and testing helicopter dynamics is a very complex problem. The problems in helicopter flight dynamics are mostly solved with the aid of modern computers. Though inevitably, with many complex problems, computers do not make it possible to understand the physical nature of the problem. Fortunately, many problems related to helicopters can be analyzed without overly complex calculus, and usually it is possible to obtain simple formulae. Though not suitable for calculus, these formulae, when designing the helicopter, enable a satisfactory interpretation of the required aerodynamic and dynamic phenomena. The helicopter belongs to the group of aerospace systems and its traditional modeling may be divided into: a) three-dimensional (space) geometry and kinematics, and b) rigid-body dynamics and the fluid dynamics through which it moves. Recently, the following models were developed: c) the elasticity model in intersubordinance with a fluid, d) the propulsion system model, e) the hydraulic model and other actuators that achieve aerodynamic control, f) the pilot-behavior model, g) the navigation-system model, and h) the beacon-problem model. The mathematical model described in this paper is related to a) and b). UR - https://www.sv-jme.eu/sl/article/mathematical-models-of-helicopter-flight-dynamics/
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author = {Cvetkovič, D., Radaković, D.},
title = {Mathematical Models of Helicopter Flight Dynamics},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {53},
number = {2},
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TY - JOUR AU - Cvetkovič, Dragan AU - Radaković, Duško PY - 2017/10/24 TI - Mathematical Models of Helicopter Flight Dynamics JF - Strojniški vestnik - Journal of Mechanical Engineering; Vol 53, No 2 (2007): Strojniški vestnik - Journal of Mechanical Engineering DO - KW - helicopters, flight dynamics, mathematical models, N2 - The helicopter is a specific form of traffic-transportation, not just in terms of its structure but also in terms of its possibilities for motion. The helicopter can move vertically, hover in the air, turn around, move forward and move laterally, and it can also perform combinations of these movements. As a result, modeling and testing helicopter dynamics is a very complex problem. The problems in helicopter flight dynamics are mostly solved with the aid of modern computers. Though inevitably, with many complex problems, computers do not make it possible to understand the physical nature of the problem. Fortunately, many problems related to helicopters can be analyzed without overly complex calculus, and usually it is possible to obtain simple formulae. Though not suitable for calculus, these formulae, when designing the helicopter, enable a satisfactory interpretation of the required aerodynamic and dynamic phenomena. The helicopter belongs to the group of aerospace systems and its traditional modeling may be divided into: a) three-dimensional (space) geometry and kinematics, and b) rigid-body dynamics and the fluid dynamics through which it moves. Recently, the following models were developed: c) the elasticity model in intersubordinance with a fluid, d) the propulsion system model, e) the hydraulic model and other actuators that achieve aerodynamic control, f) the pilot-behavior model, g) the navigation-system model, and h) the beacon-problem model. The mathematical model described in this paper is related to a) and b). UR - https://www.sv-jme.eu/sl/article/mathematical-models-of-helicopter-flight-dynamics/
Cvetkovič, Dragan, AND Radaković, Duško. "Mathematical Models of Helicopter Flight Dynamics" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 53 Number 2 (24 October 2017)
Strojniški vestnik - Journal of Mechanical Engineering 53(2007)2, 114-126
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.
The helicopter is a specific form of traffic-transportation, not just in terms of its structure but also in terms of its possibilities for motion. The helicopter can move vertically, hover in the air, turn around, move forward and move laterally, and it can also perform combinations of these movements. As a result, modeling and testing helicopter dynamics is a very complex problem. The problems in helicopter flight dynamics are mostly solved with the aid of modern computers. Though inevitably, with many complex problems, computers do not make it possible to understand the physical nature of the problem. Fortunately, many problems related to helicopters can be analyzed without overly complex calculus, and usually it is possible to obtain simple formulae. Though not suitable for calculus, these formulae, when designing the helicopter, enable a satisfactory interpretation of the required aerodynamic and dynamic phenomena. The helicopter belongs to the group of aerospace systems and its traditional modeling may be divided into: a) three-dimensional (space) geometry and kinematics, and b) rigid-body dynamics and the fluid dynamics through which it moves. Recently, the following models were developed: c) the elasticity model in intersubordinance with a fluid, d) the propulsion system model, e) the hydraulic model and other actuators that achieve aerodynamic control, f) the pilot-behavior model, g) the navigation-system model, and h) the beacon-problem model. The mathematical model described in this paper is related to a) and b).