Searched for: mods_originInfo_publisher_s%3A%22American%255C%2BInstitute%255C%2Bof%255C%2BAeronautics%255C%2Band%255C%2BAstronautics%22
(1 - 8 of 8)
- document
-
Sanna, F. (author), Golliard, J. (author)In this study experiments are conducted on the flow within a horizontal pipe with two closed side branches of equal length. This configuration is referred to as "quasi-cross configuration" as the distance between the two closed side branches is much smaller than the acoustic wavelength of the first acoustic mode. Focus is placed upon...conference paper 2014
- document
-
Brodecki, M. (author), Subbarao, K. (author), Chu, Q.P. (author)Emergent behavior of a formation flight control system based on an advanced extremum seeking algorithm is investigated. The control system was implemented on a nonlinear high fidelity aircraft model and combined with a wake vortex model in order to accurately represent the aerodynamic coupling experienced by members of a formation. The desired...conference paper 2013
- document
-
Brodecki, M. (author), Subbarao, K. (author), Chu, Q.P. (author)A formation flight control system has been designed that addresses the unique environment encountered by aircraft flying in formation and in the upwash of the leading aircraft. In order to test the control system a simulation environment has been created that adequately represents the aerodynamic coupling effects between aircraft flying in...conference paper 2013
- document
-
Correia Grácio, B.J. (author), Wentink, M. (author), Bos, J.E. (author), van Paassen, M.M. (author), Mulder, M. (author)In motion simulation, motion cueing algorithms are used to transform vehicle inertial cues into inertial cues that are within the simulator physical limits. Most motion cueing algorithms aim to minimize the error between these vehicle inertial cues and those generated by the simulator. Although this is one way to approach the problem, one can...conference paper 2012
- document
-
Correia Grácio, B.J. (author), Wentink, M. (author), Bos, J.E. (author), van Paassen, M.M. (author), Mulder, M. (author)In the field of motion simulation it was found that a visual amplitude equal to the inertial amplitude does not always provide the best perceived match between visual and inertial motion. This result is thought to be caused by the “quality” of the motion cues delivered by the simulator motion and visual systems. This paper studies how different...conference paper 2012
- document
-
Correia Grácio, B.J. (author), Valente Pais, A.R. (author), van Paassen, M.M. (author), Mulder, M. (author), Kelly, L.C. (author), Houck, J.A. (author)In motion simulation the inertial information generated by the motion platform is most of the times different from the visual information in the simulator displays. This occurs due to the physical limits of the motion platform. However, for small motions that are within the physical limits of the motion platform, one-to-one motion, i.e. visual...conference paper 2011
- document
-
Correia Grácio, B.J. (author), van Paassen, M.M. (author), Mulder, M. (author), Wentink, M. (author), TNO Defensie en Veiligheid (author)Generally, motion simulators present motion and visual cues different from each other due to the physical limitations of the motion platform. Nonetheless, high fidelity motion platforms are capable of simulating some maneuvers one-to-one, i.e., motion cues equal to visual cues. However, one-to-one simulation is normally not preferred by subjects...conference paper 2010
- document
-
de Winkel, K.N. (author), Correia Grácio, B.J. (author), Groen, E.L. (author), Werkhoven, P.J. (author), TNO Defensie en Veiligheid (author)Knowledge of human motion perception can be applied in the optimization of motion cueing algorithms. In the past it has been shown that some discrepancies between the amplitude or phase of a visual and inertial cue go unnoticed. These acceptable discrepancies are referred to as coherence zones. In the present experiment we investigate whether a...conference paper 2010
Searched for: mods_originInfo_publisher_s%3A%22American%255C%2BInstitute%255C%2Bof%255C%2BAeronautics%255C%2Band%255C%2BAstronautics%22
(1 - 8 of 8)