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Flight simulation in flight dynamics education
24th Atmospheric Flight Mechanics Conference, 1999Thii paper describes the use of manned Sight simulation for flight dynamics education. The uses of a simulator for instruction and some of the capabilities that make these uses possible are discussed. Specific examples of the use of simulation in classes in the Virginia Tech Aerospace Engineering curriculum are presented.
Roger Beck, Wayne Durham
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2020 International Conference on Virtual Reality and Visualization (ICVRV), 2020
This article introduces a dynamic flight simulator. The dynamic flight simulator is composed of three-degree-of-freedom platform, flight seat, flight stick, VR glasses, physical simulation platform and other equipment. Experienced people operate the flight joystick, and can experience realistic flight vision through VR glasses.
Jinpeng Zhang +2 more
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This article introduces a dynamic flight simulator. The dynamic flight simulator is composed of three-degree-of-freedom platform, flight seat, flight stick, VR glasses, physical simulation platform and other equipment. Experienced people operate the flight joystick, and can experience realistic flight vision through VR glasses.
Jinpeng Zhang +2 more
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AIAA Atmospheric Flight Mechanics Conference, 2011
Tensor flight dynamics models flight dynamics with Cartesian tensors that are invariant under all coordinate transformations, even time dependent transformations. It elevates Newton’s Second Law to a law that is not only invariant under inertial coordinate transformations, but under all transformations, thus bringing Newtonian mechanics under the ...
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Tensor flight dynamics models flight dynamics with Cartesian tensors that are invariant under all coordinate transformations, even time dependent transformations. It elevates Newton’s Second Law to a law that is not only invariant under inertial coordinate transformations, but under all transformations, thus bringing Newtonian mechanics under the ...
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2011
All research activities related to flight dynamics, aerodynamics and thermodynamics are grouped under the ARCHYFLOW sub-program, which stands for ARCHIMEDES Hypersonic Flight and Low speed descent. ARCHYFLOW analyses were performed starting with 3D trajectory simulations [39], including steady state [40] and transient [41] thermal analyses.
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All research activities related to flight dynamics, aerodynamics and thermodynamics are grouped under the ARCHYFLOW sub-program, which stands for ARCHIMEDES Hypersonic Flight and Low speed descent. ARCHYFLOW analyses were performed starting with 3D trajectory simulations [39], including steady state [40] and transient [41] thermal analyses.
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The JWST Flight Dynamics Operations Concept and Flight Dynamics Ground System
2020 IEEE Aerospace Conference, 2020The James Webb Space Telescope (JWST) Flight Dynamics Team (FDT), operating from the NASA Goddard Space Flight Center (GSFC) Flight Dynamics Facility (FDF), is responsible for providing orbit determination (OD), trajectory predictions, view period predictions, and maneuver planning, monitoring, reconstruction, and calibration. The FDT delivers products
Joshua Levi +3 more
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2011
To present the basic flight dynamics modeling approach applicable to aircraft, rockets, and spacecraft. To derive the equations of motion for typical flight dynamic systems. To describe the sensors used in flight control systems.
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To present the basic flight dynamics modeling approach applicable to aircraft, rockets, and spacecraft. To derive the equations of motion for typical flight dynamic systems. To describe the sensors used in flight control systems.
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Flight Display Dynamics Revisited
Human Factors: The Journal of the Human Factors and Ergonomics Society, 1981Good old ideas for pictorial flight displays that were once impractical warrant reconsideration in light of current microcomputing and display technology. Among the ideas are the contact analog, highway in the sky, and flight path predictor concepts.
Stanley N. Roscoe +2 more
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2011
In Chap. 6, we present a comprehensive modeling process to obtain a highly accurate nonlinear dynamical model for our unmanned systems, SheLion (also applicable to HeLion). We first derive a minimum-complexity model structure, which covers all the important dynamic features necessary for flight control law design.
Guowei Cai, Ben M. Chen, Tong Heng Lee
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In Chap. 6, we present a comprehensive modeling process to obtain a highly accurate nonlinear dynamical model for our unmanned systems, SheLion (also applicable to HeLion). We first derive a minimum-complexity model structure, which covers all the important dynamic features necessary for flight control law design.
Guowei Cai, Ben M. Chen, Tong Heng Lee
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30th AIAA Applied Aerodynamics Conference, 2012
Aerodynamic characteristics and flight dynamics of boomerangs are investigated. A basic aerodynamic model, developed in the 1960’s, is expanded upon using Blade Element Theory. The new aerodynamic model is coupled with a gyroscope model for rudimentary analyses.
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Aerodynamic characteristics and flight dynamics of boomerangs are investigated. A basic aerodynamic model, developed in the 1960’s, is expanded upon using Blade Element Theory. The new aerodynamic model is coupled with a gyroscope model for rudimentary analyses.
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