Searched for: subject%3A%22simulations%22
(1 - 20 of 39)

Pages

List view
Grid view
document
Scaramuzzino, Paolo Francesco (author)
This research aims to advance the state-of-the-art requirements for helicopter pilot training in flight simulators contributing to the rotorcraft safety enhancement framework. It has been conducted as part of the Marie Sk\l odowska-Curie European Joint Doctorate NITROS (Network for Innovative Training on Rotorcraft Safety).<br/><br/>Training has...
doctoral thesis 2022
document
Miletović, I. (author)
Flight simulators, or Flight Simulation Training Devices (FSTDs), offer great benefits in terms of safety and cost associated with pilot training and certification. To warrant uniform certification standards and to prevent adverse pilot training, (sub)system fidelity requirements are imposed by the Federal Aviation Authority (FAA) and European...
doctoral thesis 2020
document
Landman, H.M. (author), van Oorschot, P. (author), van Paassen, M.M. (author), Groen, Eric L. (author), Bronkhorst, Adelbert W. (author), Mulder, Max (author)
Objective: This study tested whether simulator-based training of pilot responses to unexpected or novel events can be improved by including unpredictability and variability in training scenarios. Background: Current regulations allow for highly predictable and invariable training, which may not be sufficient to prepare pilots for unexpected...
journal article 2018
document
Valente Pais, A.R. (author)
A perception coherence zone (PCZ) designates the range of inertial motion levels that, although not being a one-to-one match with the visual motion levels, are still considered by the subjects as being part of a coherent movement. Two types of PCZs were studied: amplitude PCZs and phase PCZs. Amplitude and phase coherences zones were measured...
doctoral thesis 2013
document
Pool, D.M. (author)
Compared to aircraft, flight simulators are severely limited in their motion envelopes. Presenting the true aircraft motion one-to-one on flight simulators is generally impossible and it is therefore common practice that these motion stimuli are only presented in reduced and attenuated form. Because of a limited understanding of human motion...
doctoral thesis 2012
document
Brijl, B.R. (author)
Vertigo Flight Simulation is a company located in The Netherlands with its mission being to design, produce and sell low cost flight simulation devices to all levels of the flight training market. One of the products which is developed by Vertigo Flight Simulation is the Vertigo P-2 Trainer. The P-2 Trainer is a fixed-base flight simulator...
master thesis 2003
document
Koekebakker, S.H. (author)
doctoral thesis 2001
document
Torenbeek, E. (author)
book 1998
document
van Gent, R.N.H.W. (author)
The experiments described had three main objectives: First, to validate the recommendations for an improved Man Machine Interface (MMI) design based on a Phase I experiment on the human factors of data link in glass cockpits. Second, to investigate the effect of directly loading data linked Air Traffic Control (ATC) instructions into the various...
report 1995
document
ten Dam, A.A. (author), Schrap, F. (author), Brouwer, W. (author)
The Programme and Real-time Operations SIMulation support tool PROSIM is a generic simulation tool that can be used for design, verification, test and training of a wide range of applications, such as aircraft and groimd vehicles. PROSIM originated as part of the National Simulation Facility NSF at the Dutch National Aerospace Laboratoiy NLR, a...
report 1994
document
Mooij, E. (author)
report 1994
document
Wanhill, R.J.H. (author)
Flight simulation fatigue crack growth tests are necessary for verification of aircraft damage tolerance analyses and crack growth prediction methods, and also for comparing candidate materials for aircraft structural applications. However, such tests involve complicating issues that have emerged from many investigations on aluminium alloys...
report 1993
document
Mooij, E. (author), Maree, A.G.M. (author), Zandbergen, B.T.C. (author)
report 1993
document
van der Hoeven, W. (author)
Residual strength tests were performed on ARALL panels consisting of ARALL3 (3/2) laminates with bonded-on doublers. In particular, the effect of the doubler geometry (shape and thickness) on the residual strength was investigated. Prior to residual strength testing all panels were fatigue loaded to create a realistic type of damage, i.e. cracks...
report 1992
document
Schra, L. (author), Wanhill, R.J.H. (author)
Flight simulation fatigue growth tests were done on 1.6 mm thick sheets of the damage tolerant aluminium-lithium (Al-Li) alloys 2091-T84 and 8090-T81 in comparison with the industry standard conventional damage tolerant alloy 2024-T3. The flight simulation load spectrum, the gust spectrum MINITWIST, was used in four versions: untruncated,...
report 1991
document
Erkelens, L.J.J. (author), van Dronkelaar, J.H. (author)
The flight simulator study described In this report concerns an evaluation of flight director flown curved MLS approach paths with a simulated wide-body transport aircraft. Four curved approach paths, consisting of two straight segments and one 90 degrees circular segment with different straight final segment lengths, have been investigated....
report 1990
document
ten Have, A.A. (author)
Typical characteristics of various types of service loading are presented as they were discussed during the establishment of standardised test load sequences. Counting methods are reviewed and a simple and powerful algorithm is given to perform rainflow counting and to store the counting results afterwards. Synthesis procedures are discussed...
report 1987
document
van der Linden, H.H. (author)
The report contains the description, results and conclusions of a fatigue test programme which assessed the fatigue lives of fastener systems using different joints. High load transfer single shear joints were evaluated in a core programme; secondary bending and load transfer were determined experimentally. About 750 specimens were fatigue...
report 1985
document
van Gool, M.F.C. (author), Rickard, W.W. (author)
Future transport aircraft will be different from to-day's in that they will be designed to be statically neutrally stable or even unstable to improve economics, while the stability will be provided by means of a fly-by-wire flight control system. Since this system will be flight critical it is necessary to develop a philosophy on the treatment...
report 1984
document
Schijve, J. (author), Jacobs, F.A. (author)
Fatigue tests were carried out on Redux and FM 123/5 bonded specimens at various stress levels, temperatures (RT to 65 C) and low and high test frequencies. Observations were made on the type of failure (bond line failure or sheet failure) and the significance of the adhesive squeezeout for crack nucleation. An analysis of the data and a...
report 1984
Searched for: subject%3A%22simulations%22
(1 - 20 of 39)

Pages

List view
Grid view