Academic literature on the topic 'Vertically rising airplanes'

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Journal articles on the topic "Vertically rising airplanes"

1

Gradolewski, Dawid, Damian Dziak, Damian Kaniecki, Adam Jaworski, Michal Skakuj, and Wlodek J. Kulesza. "A Runway Safety System Based on Vertically Oriented Stereovision." Sensors 21, no. 4 (February 20, 2021): 1464. http://dx.doi.org/10.3390/s21041464.

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In 2020, over 10,000 bird strikes were reported in the USA, with average repair costs exceeding $200 million annually, rising to $1.2 billion worldwide. These collisions of avifauna with airplanes pose a significant threat to human safety and wildlife. This article presents a system dedicated to monitoring the space over an airport and is used to localize and identify moving objects. The solution is a stereovision based real-time bird protection system, which uses IoT and distributed computing concepts together with advanced HMI to provide the setup’s flexibility and usability. To create a high degree of customization, a modified stereovision system with freely oriented optical axes is proposed. To provide a market tailored solution affordable for small and medium size airports, a user-driven design methodology is used. The mathematical model is implemented and optimized in MATLAB. The implemented system prototype is verified in a real environment. The quantitative validation of the system performance is carried out using fixed-wing drones with GPS recorders. The results obtained prove the system’s high efficiency for detection and size classification in real-time, as well as a high degree of localization certainty.
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Wilga, C. D., and G. V. Lauder. "Three-dimensional kinematics and wake structure of the pectoral fins during locomotion in leopard sharks Triakis semifasciata." Journal of Experimental Biology 203, no. 15 (August 1, 2000): 2261–78. http://dx.doi.org/10.1242/jeb.203.15.2261.

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The classical theory of locomotion in sharks proposes that shark pectoral fins are oriented to generate lift forces that balance the moment produced by the oscillating heterocercal tail. Accordingly, previous studies of shark locomotion have used fixed-wing aircraft as a model assuming that sharks have similar stability and control mechanisms. However, unlike airplanes, sharks are propelled by undulations of the body and tail and have considerable control of pectoral fin motion. In this paper, we use a new approach to examine the function of the pectoral fins of leopard sharks, Triakis semifasciata, during steady horizontal swimming at speeds of 0.5-2.0ls(−1), where l is total body length, and during vertical maneuvering (rising and sinking) in the water column. The planar orientation of the pectoral fin was measured using three-dimensional kinematics, while fluid flow in the wake of the pectoral fin and forces exerted on the water by the fin were quantified using digital particle image velocimetry (DPIV). Steady horizontal swimming in leopard sharks is characterized by continuous undulations of the body with a positive body tilt to the flow that decreases from a mean of 11 degrees to 0.6 degrees with increasing flow speeds from 0. 5 to 2.0ls(−1). Three-dimensional analysis showed that, during steady horizontal locomotion, the pectoral fins are cambered, concave downwards, at a negative angle of attack that we predict to generate no significant lift. Leopard shark pectoral fins are also oriented at a substantial negative dihedral angle that amplifies roll moments and hence promotes rapid changes in body position. Vortices shed from the trailing edge of the pectoral fin were detected only during vertical maneuvering. Starting vortices are produced when the posterior plane of the pectoral fin is actively flipped upwards or downwards to initiate rising or sinking, respectively, in the water column. The starting vortex produced by the pectoral fin induces a pitching moment that reorients the body relative to the flow. Body and pectoral fin surface angle are altered significantly when leopard sharks change vertical position in the water column. Thus, locomotion in leopard sharks is not analogous to flight in fixed-wing aircraft. Instead, a new force balance for swimming leopard sharks is proposed for steady swimming and maneuvering. Total force balance on the body is adjusted by altering the body angle during steady swimming as well as during vertical maneuvering, while the pectoral fins appear to be critical for initiating maneuvering behaviors, but not for lift production during steady horizontal locomotion.
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Dissertations / Theses on the topic "Vertically rising airplanes"

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Hunsaker, Douglas F. "A Numerical Vortex Approach To Aerodynamic Modeling of SUAV/VTOL Aircraft." Diss., CLICK HERE for online access, 2007. http://contentdm.lib.byu.edu/ETD/image/etd1678.pdf.

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Knoebel, Nathan B. "Adaptive Quaternion Control for a Miniature Tailsitter UAV." Diss., CLICK HERE for online access, 2007. http://contentdm.lib.byu.edu/ETD/image/etd2092.pdf.

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Books on the topic "Vertically rising airplanes"

1

Rogers, Mike. VTOL military research aircraft. Sparkford, Nr. Yeovil, Somerset: Haynes, 1989.

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VTOL military research aircraft. New York: Orion Books, 1989.

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Myhra, David. Dragonfly: The Luftwaffe's experimental Triebflü̈geljäger Project. Atglen, PA: Schiffer Pub., 2000.

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Albers, James A. Aircraft technology opportunities for the 21st century. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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Riley, Donald R. Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept. Hampton, Va: Langley Research Center, 1989.

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Riley, Donald R. Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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Riley, Donald R. Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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Vogt, William G. Computer simulation of a pilot in V/STOL aircraft control loops: Final report for NASA grant NAG 3-729. Cleveland, OH: NASA Lewis Research Center, 1989.

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Vogt, William G. Computer simulation of a pilot in V/STOL aircraft control loops. Cleveland, OH: NASA Lewis Research Center, 1989.

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Vogt, William G. Computer simulation of a pilot in V/STOL aircraft control loops. Cleveland, OH: NASA Lewis Research Center, 1988.

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