An envelope protection scheme is proposed for responding to a microburst. This approach is based on limiting the allowable maximum inertial deceleration of the aircraft when flying at low airspeeds. This technique is shown in simulations to be very effective at preventing stall and resulting in minimal loss of altitude. It is speculated that the same scheme can also protect an aircraft in the event of other forms of windshear encounters, such as making a sudden turn to downwind.
Response of an Advanced Flight Control System to Microburst Encounters
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 2005
2005-10-03
Aufsatz (Konferenz)
Englisch
of an Advanced Flight Control System to Microburst Encounters
British Library Conference Proceedings | 2005
|Lateral Escape Guidance Strategies for Microburst Windshear Encounters
Online Contents | 1997
|Lateral Escape Guidance Strategies for Microburst Windshear Encounters
British Library Conference Proceedings | 1997
|