MPCA for flight dynamics parameters determination

Journal Title: Computer Assisted Methods in Engineering and Science - Year 2014, Vol 21, Issue 3

Abstract

Aircraft have become increasingly costly and complex. Military and civil pilots and engineers have used flight simulators in order to increase safety of flight through the training of crew. It is necessary to calibrate the simulation for simulators to have good adherence to reality, that is, to identify the parameters that make the simulation as close as possible to the actual dynamics. After determining these parameters, the simulator will be ready to be used in human resources training or assessing the aircraft. Parameter identification characterizes the aerodynamic performance of the aircraft and can be formulated as a problem optimization. The calibration of a dynamic flight simulator is achieved by a new meta-heuristic called multiple particle collision algorithm (MPCA). Preliminary results show a good performance of the employed approach.

Authors and Affiliations

Ivana Y. Sumida, Haroldo F. de Campos Velho, Eduardo F. P. Luz, Ronaldo V. Cruz, Luiz Carlos S. Góes

Keywords

Related Articles

A shift-add algorithm for generating B-spline

A CORDIC- based shift-add algorithm for generating B-spline curves is presented in this paper. This algorithm can be realized by hardware without multiplier, or coded with assembly language and run in the basic computing...

Inverse problem in anomalous diffusion with uncertainty propagation

Recently, Bevilacqua, Galeão and co-workers have developed a new analytical formulation for the simulation of diffusion with retention phenomena. This new formulation aims at the reduction of all diffusion processes with...

Identification of electron-phonon coupling factor in a thin metal film subjected to an ultrashort laser pulse

A thin metal film subjected to a laser pulse is considered. The problem is described by the system of energy equations describing the electron gas and lattice temperatures. The thermal interactions between electrons and...

Coupling of CFD and lumped parameter codes for thermal-hydraulic simulations of reactor containment

The work deals with thermal-hydraulic analyses of a pressurized water reactor containment response to accidents caused by a rupture of primary circuit. The in-house system computer code HEPCAL-AD and CFD ANSYS Fluent hav...

Modelling dynamics of transmission conductors with Cosserat rod

We proposed a method to analyze the galloping, a vibration by wind force, of transmission conductors. The Cosserat rod model was introduced to describe the motion of the conductor line. The deformation was tracked using...

Download PDF file
  • EP ID EP73505
  • DOI -
  • Views 200
  • Downloads 0

How To Cite

Ivana Y. Sumida, Haroldo F. de Campos Velho, Eduardo F. P. Luz, Ronaldo V. Cruz, Luiz Carlos S. Góes (2014). MPCA for flight dynamics parameters determination. Computer Assisted Methods in Engineering and Science, 21(3), 257-265. https://europub.co.uk/articles/-A-73505