Calculation of the acceleration force components and roll and pitch link angles of the CFS and SDT
Abstract
Pilots of modern combat aircraft are exposed to the devastating effects of high acceleration
forces and unusual orientation. The pilots’ ability to perform tasks under these extreme flight
conditions must be examined. A centrifuge flight simulator (CFS) for pilot training is designed as
a three-degree-of-freedom 3DoF manipulator with rotational axes. Through rotations about these
axes, acceleration forces that act on aircraft pilots are simulated. The spatial disorientation trainer
(SDT) examines a pilot’s ability to recognise unusual orientations, to adapt to unusual positions
and to persuade the pilot to believe in the aircraft instruments for orientation and not in his own
senses. The SDT is designed as a (4DoF) manipulator with rotational axes. Through rotations
about these axes, different orientations can be achieved; different acceleration forces acting on the
pilot can also be simulated. In this paper, the acceleration forces and angular velocities that act on
the simu...lator pilot in the CMS and SDT are calculated along with the roll and pitch angles of the
gondola for these forces.
Keywords:
Centrifuge flight simulator / Spatial disorientation trainer / Kinematics / Dynamics / Control algorithm / RoboticsSource:
6th International Congress of Serbian Society of Mechanics, Tara, Serbia, June 19-21, 2017, 2017, 1-10Publisher:
- Beograd : Srpsko društvo za mehaniku
Funding / projects:
- Development of devices for pilot training and dynamic flight simulation of modern fighter aircrafts: 3DoF centrifuge and 4DoF spatial disorientation trainer (RS-MESTD-Technological Development (TD or TR)-35023)
- Sustainability and improvement of mechanical systems in energetic, material handling and conveying by using forensic engineering, environmental and robust design (RS-MESTD-Technological Development (TD or TR)-35006)
Collections
Institution/Community
Mašinski fakultetTY - CONF AU - Kvrgić, Vladimir AU - Vidaković, Jelena AU - Lazarević, Mihailo AU - Pavlović, Goran PY - 2017 UR - https://machinery.mas.bg.ac.rs/handle/123456789/4146 AB - Pilots of modern combat aircraft are exposed to the devastating effects of high acceleration forces and unusual orientation. The pilots’ ability to perform tasks under these extreme flight conditions must be examined. A centrifuge flight simulator (CFS) for pilot training is designed as a three-degree-of-freedom 3DoF manipulator with rotational axes. Through rotations about these axes, acceleration forces that act on aircraft pilots are simulated. The spatial disorientation trainer (SDT) examines a pilot’s ability to recognise unusual orientations, to adapt to unusual positions and to persuade the pilot to believe in the aircraft instruments for orientation and not in his own senses. The SDT is designed as a (4DoF) manipulator with rotational axes. Through rotations about these axes, different orientations can be achieved; different acceleration forces acting on the pilot can also be simulated. In this paper, the acceleration forces and angular velocities that act on the simulator pilot in the CMS and SDT are calculated along with the roll and pitch angles of the gondola for these forces. PB - Beograd : Srpsko društvo za mehaniku C3 - 6th International Congress of Serbian Society of Mechanics, Tara, Serbia, June 19-21, 2017 T1 - Calculation of the acceleration force components and roll and pitch link angles of the CFS and SDT EP - 10 SP - 1 UR - https://hdl.handle.net/21.15107/rcub_machinery_4146 ER -
@conference{ author = "Kvrgić, Vladimir and Vidaković, Jelena and Lazarević, Mihailo and Pavlović, Goran", year = "2017", abstract = "Pilots of modern combat aircraft are exposed to the devastating effects of high acceleration forces and unusual orientation. The pilots’ ability to perform tasks under these extreme flight conditions must be examined. A centrifuge flight simulator (CFS) for pilot training is designed as a three-degree-of-freedom 3DoF manipulator with rotational axes. Through rotations about these axes, acceleration forces that act on aircraft pilots are simulated. The spatial disorientation trainer (SDT) examines a pilot’s ability to recognise unusual orientations, to adapt to unusual positions and to persuade the pilot to believe in the aircraft instruments for orientation and not in his own senses. The SDT is designed as a (4DoF) manipulator with rotational axes. Through rotations about these axes, different orientations can be achieved; different acceleration forces acting on the pilot can also be simulated. In this paper, the acceleration forces and angular velocities that act on the simulator pilot in the CMS and SDT are calculated along with the roll and pitch angles of the gondola for these forces.", publisher = "Beograd : Srpsko društvo za mehaniku", journal = "6th International Congress of Serbian Society of Mechanics, Tara, Serbia, June 19-21, 2017", title = "Calculation of the acceleration force components and roll and pitch link angles of the CFS and SDT", pages = "10-1", url = "https://hdl.handle.net/21.15107/rcub_machinery_4146" }
Kvrgić, V., Vidaković, J., Lazarević, M.,& Pavlović, G.. (2017). Calculation of the acceleration force components and roll and pitch link angles of the CFS and SDT. in 6th International Congress of Serbian Society of Mechanics, Tara, Serbia, June 19-21, 2017 Beograd : Srpsko društvo za mehaniku., 1-10. https://hdl.handle.net/21.15107/rcub_machinery_4146
Kvrgić V, Vidaković J, Lazarević M, Pavlović G. Calculation of the acceleration force components and roll and pitch link angles of the CFS and SDT. in 6th International Congress of Serbian Society of Mechanics, Tara, Serbia, June 19-21, 2017. 2017;:1-10. https://hdl.handle.net/21.15107/rcub_machinery_4146 .
Kvrgić, Vladimir, Vidaković, Jelena, Lazarević, Mihailo, Pavlović, Goran, "Calculation of the acceleration force components and roll and pitch link angles of the CFS and SDT" in 6th International Congress of Serbian Society of Mechanics, Tara, Serbia, June 19-21, 2017 (2017):1-10, https://hdl.handle.net/21.15107/rcub_machinery_4146 .