Mathematical Models of Helicopter Flight Dynamics

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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: 05 dec. 2021. 
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.  05 Dec. 2021
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/
@article{{}{.},
	author = {Cvetkovič, D., Radaković, D.},
	title = {Mathematical Models of Helicopter Flight Dynamics},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {53},
	number = {2},
	year = {2007},
	doi = {},
	url = {https://www.sv-jme.eu/sl/article/mathematical-models-of-helicopter-flight-dynamics/}
}
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)

Avtorji

Inštitucije

  • University "Union" Faculty of Computer Science, Belgrade, Serbia
  • Federal Bureau for Measures and Precious Metals, Belgrade, Serbia

Informacije o papirju

Strojniški vestnik - Journal of Mechanical Engineering 53(2007)2, 114-126

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).

helicopters; flight dynamics; mathematical models;