AIAA Modeling and Simulation Technologies Conference 2012
DOI: 10.2514/6.2012-4631
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Cited by 20 publications
(19 citation statements)
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“…Different statistical surveys reported (see, for example, [1]) that loss of control in flight (LOC-I) was the major cause of fatal transport aviation accidents. Thus, many intensive studies are aimed at modeling of aerodynamics in the extended flight envelope in order to support investigations of aircraft dynamics, control system design [2] and to provide realistic pilot training using ground-based simulators in upset conditions [3,4].…”
Section: Introductionmentioning
confidence: 99%
See 2 more Smart Citations
“…Different statistical surveys reported (see, for example, [1]) that loss of control in flight (LOC-I) was the major cause of fatal transport aviation accidents. Thus, many intensive studies are aimed at modeling of aerodynamics in the extended flight envelope in order to support investigations of aircraft dynamics, control system design [2] and to provide realistic pilot training using ground-based simulators in upset conditions [3,4].…”
Section: Introductionmentioning
confidence: 99%
“…Growth in computing capacity and the development of numerical techniques has recently led to significant progress in finding solutions for Navier-Stokes equations coupled with the dynamics equations governing the aircraft motion, facilitating flight dynamics studies [3,[5][6][7][8][9][10]. However, at present the problems of fluid mechanics and flight dynamics cannot be solved simultaneously in certain flight mechanical applications-for example, in semi-realistic simulation of the aircraft flight using ground-based flight simulators or control system design [3,11].…”
Section: Introductionmentioning
confidence: 99%
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“…However this analysis has largely focused on military aircraft. This approach has recently been implemented, for commercial airliners, on the NASA Generic Transport Model (GTM) [13] and the SUPRA model [10] in open-loop form, and has revealed spiral dives and steep spins. This paper extends the bifurcation analysis performed in [13] to analyse the dynamics of the GTM coupled to closed loop controllers.…”
Section: Introductionmentioning
confidence: 99%
“…The purpose of the model, derived from a comprehensive wind tunnel test campaign as well as from remotely piloted tests of a powered flight vehicle, was indeed to generate a representative wide-envelope airliner flight dynamics model for the simulation and analysis of upset and LOC [9]. A similar model was created for the EU 'Simulation of UPset Recovery in Aviation' (SUPRA) research programme [10].…”
Section: Introductionmentioning
confidence: 99%