Modeling Flight Through Clear Air Turbulence

Torgerson, Joshua F.; Walker, Michael M.; Kopeikin, Andrew; Jumper, George Y.

doi:10.2514/6.2006-73

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U-2 Simulation1

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Cited by 5 publications

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“…In this method, the forces and moment are calculated using a first order expansion, in which each state variable makes a contribution to the total force proportional to the stability derivative. This simulation formulation is identical to the one utilized for an Egrett aircraft investigation, given at the 2006 AIAA conference [3].…”

Section: U-2 Simulationmentioning

confidence: 99%

Modeling U-2 Flight Through Clear Air Turbulence

Torgerson

Walker

Kopeikin

et al. 2007

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Section: U-2 Simulationmentioning

confidence: 99%

Modeling U-2 Flight Through Clear Air Turbulence

Torgerson

Walker

Kopeikin

et al. 2007

View full text Add to dashboard Cite

“…There are two basic approaches in processing FDR data to infer related aerodynamic information that can provide more insides regarding flight accidents. The first approach requires suitable flight dynamic and sensor models and related partials [Weng, et al, 2006] while the second one relies on establishing correct relationship between input and output parameters using neural network based algorithm [Peyada and Ghosh, 2009;Singh, 2005;Torgerson, et al, 2006]. The outcomes of FDR data processing can be used to evaluate flight conditions.…”

Section: Introductionmentioning

confidence: 99%