In the past, there have been a number of fatal incidents attributable to wake vortex encounters, involving both general aviation and commercial aircraft. In fact, the wake vortex hazard is considered to be the single dominant safety issue determining the aircraft spacing requirements at airports. As the amount of air traffic increases, the number of dangerous encounters is likely only to increase. It is therefore imperative that a means be found to reduce the danger. That is the purpose of this research: to use nonlinear inverse dynamic (NID) control methods in the design of an aircraft control system which can improve the safety margin in a wake vortex encounter.
Aircraft control in wake vortex wind shear
1995-08-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aircraft Control in Wake Vortex Wind Shear
British Library Conference Proceedings | 1995
|Aircraft Control in Wake Vortex Wind Shear
NTIS | 1995
|SAE Technical Papers | 1996
|Wind shear and vortex wake research in UK, 1982
NTRS | 1982
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