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    Optimal trajectory planning for flight through microburst wind shears

    , Article Aerospace Science and Technology ; Volume 15, Issue 7 , October , 2011 , Pages 567-576 ; 12709638 (ISSN) Pourtakdoust, S. H ; Kiani, M ; Hassanpour, A ; Sharif University of Technology
    2011
    Abstract
    Microburst wind shear is a potential hazard for aviation safety, especially in some crucial phases of flight like take-off and landing. Optimal trajectories could be useful for suitable retrieval of transport aircrafts encountering microburst. These types of trajectories are investigated in this paper for landing phase in two scenarios of escape and landing utilizing the most recent realistic analytical model of the microburst. In this regard, a set of complete six degrees of freedom aircraft's equations of motion is taken in a variation formulation of this problem. This approach is particularly useful for determination of optimal escape or approach trajectories constrained with respect to... 

    Optimal-time quadcopter descent trajectories avoiding the vortex ring and autorotation states

    , Article Mechatronics ; Volume 68 , 2020 Talaeizadeh, A ; Antunes, D ; Nejat Pishkenari, H ; Alasty, A ; Sharif University of Technology
    Elsevier Ltd  2020
    Abstract
    It is well-known that helicopters descending fast may enter the so-called Vortex Ring State (VRS), a region in the velocity space where the blade's lift differs significantly from regular regions and high amplitude fluctuations are often present. These fluctuations may lead to instability and, therefore, this region is avoided, typically by increasing the horizontal speed. This paper researches this phenomenon in the context of small-scale quadcopters. The region corresponding to the VRS is identified by combining first-principles modeling and wind-tunnel experiments. Moreover, we propose that the so-called Windmill-Brake State (WBS) or autorotation region should also be avoided for...