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Response of an Advanced Flight Control System to Microburst Encounters
Technical Paper
2005-01-3420
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
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.
Authors
Citation
Rokhsaz, K., Steck, J., Chandramohan, R., and Singh, B., "Response of an Advanced Flight Control System to Microburst Encounters," SAE Technical Paper 2005-01-3420, 2005, https://doi.org/10.4271/2005-01-3420.Also In
References
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