Control systems of moving objects at formation of estimates of dynamic properties of flying vehicles in longitudinal motion

Abstract

The problem of synthesis of control of longitudinal motion of a flying vehicle under the action of step signal of increment of required normal overload is considered. The control is determined according to the required quality indices of transition processes. The problem is solved for essentially nonlinear dependences of aerodynamic characteristics of the flying vehicle with account of limit relations for the velocity and the elevator deflection angle. Examples of calculations of control processes for longitudinal motion are given and analyzed.