%0 Journal Article
%T Flight Transient Estimation of VTOL Aircraft with Propellers
%A Nickolay Zosimovych
%J Advances in Aerospace Science and Technology
%P 85-95
%D 2022
%I 
%R 10.4236/aast.2022.71005
%X Methodological issues associated with </span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">the </span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">determination
of the vertical</span></span></span><span><span><span style=\"font-family:&quot;\"><span style=\"font-family:Verdana;\"> take-off </span><span style=\"font-family:Verdana;\">and landing aerodynamic parameters equipped </span></span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">with </span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">two
rotary propellers </span></span></span><span><span><span style=\"font-family:&quot;\"><span style=\"font-family:Verdana;\">during </span><span style=\"font-family:Verdana;\">take-off and hovering, descent and landing are studied
in </span></span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">the </span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">proposed article. During the computer
simulation</span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"> process,</span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"> kinematic</span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">s</span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"> parameters diagrams</span></span></span><span><span><span style=\"font-family:&quot;\"> </span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">w</span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">ere</span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"> made</span></span></span><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\"><span style=\"font-family:Verdana;\">,</span></span></span><span><span><span
%K Vertical Take-Off and Landing (VTOL) Drone
%K Propeller
%K Transient
%K Thrust
%K Vector
%K Modeling
%K Kinematic
%K Aerodynamic Coefficient
%U http://www.scirp.org/journal/PaperInformation.aspx?PaperID=116239