Our previous study shows that the lateral disturbance motion of a model drone fly does not have inherent stability (passive stability),because of the existence of an unstable divergence mode.But drone flies are observed to fly stably.Constantly active control must be applied to stabilize the flight.In this study,we investigate the lateral stabilization control of the model drone fly.The method of computational fluid dynamics is used to compute the lateral control derivatives and the techniques of eigenvalue and eigenvector analysis and modal decomposition are used for solving the equations of motion.Controllability analysis shows that although inherently unstable,the lateral disturbance motion is controllable.By feeding back the state variables (i.e.lateral translation velocity,yaw rate,roll rate and roll angle,which can be measured by the sensory system of the insect) to produce anti-symmetrical changes in stroke amplitude and/or in angle of attack between the left and right wings,the motion can be stabilized,explaining why the drone flies can fly stably even if the flight is passively unstable.
The aim of this paper is to evaluate the effects ofuncertain-but-bounded parameters on the dynamic responseof structures. By combining the interval mathematics and thefinite element analysis, the mass matrix, damping matrix,stiffness matrix and the external loads are represented asinterval matrices and vector. With the help of the optimizationtheory, we present the vertex solution theorem fordetermining both the exact upper bounds or maximum valuesand the exact lower bounds or minimum values of thedynamic response of structures, in which these parametersreach their extreme values on the boundary of the intervalmass, damping, stiffness matrices and the interval externalloads vector. Three examples are used to illustrate the computationalaspects of the presented vertex solution theorem.
Zhiping Qiu Xiaojun Wang Institute of Solid Mechanics, Beihang University, 100083 Beijing, China
