Abstract

The detection of slope change points in wind curves depends on linear curve-fitting. Hall and Titterington’s algorithm based on smoothing is adapted and compared to a Bayesian method of curve-fitting. After prior spline smoothing of the data, the algorithms are tested and the errors between the split-linear fitted wind and the real one are estimated. In our case, the adaptation of the edge-preserving smoothing algorithm gives the same good performance as automatic Bayesian curve-fitting based on a Monte Carlo Markov chain algorithm yet saves computation time.

Highlights

  • This study is aimed at the improvement of the aircraft autopilot conception process

  • We focus on the effect of the linear wind components in the last 30 seconds to show that they are a decisive factor in touchdown precision. This is achieved by comparing simulated landings with either a real wind or its piecewise linear approximation. This has led us to develop a method of split-linear fitting based on slope change detection adapted to our data

  • Note that the quality of fit is measured by the MSE since, as already explained, it is impossible to replace the criterion by the one we focus on, that is difference between touchdown with the fitted wind curves and the real ones

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Summary

Introduction

This study is aimed at the improvement of the aircraft autopilot conception process. The autopilot allows landings in bad weather conditions and must guarantee passengers safety, touchdown comfort, and precision. This is achieved by comparing simulated landings with either a real wind or its piecewise linear approximation This has led us to develop a method of split-linear fitting based on slope change detection adapted to our data. The criteria to be met are estimation of a parsimonious model by detecting only the significant slope changes in the curve and achievement of the same landing properties with the real wind and with the split-linear approximation. This is an important feature of this paper, which especially involves adaptations of the algorithms which consist in prior smoothing of the data and algorithm refinements.

Aeronautical Context and Data Transformations
Split-linear Fitting Algorithms
Variation on Hall and Titterington algorithm
Bayesian automatic curve-fitting
Practical Comparisons
Estimation of error
Discussion

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