Disturbed motion of VTOL aircraft about its center of gravity, all rotation components being automatically stabilized; it is assumed that pilot constrains kinematic parameters of translation; stability of this dynamical system taking into account lag of automatic control; mathematical treatment of problem and simplified operational procedure for determining region of asymptotic stability of parameters in space.
Problems of stability of VTOL aircrafts in hovering flight
Rev de Mecanique Appliquee
Revue de Mecanique Appliquee Appliquee ; 7 , n 2
1962
15 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.