Nonlinear Control of an Aeronautical Pneumatic System

Observer-based tracking control for single machine infinite bus system via flatness theory

“…The construction of the feedback law is done by a simple inversion of system equations with respect to the system input. Although this technique has been applied to several nonlinear and linear mechanical systems [21][22][23], its application to the control of power systems has been limited to a few works [24][25][26] and [27]. However, the previous works have not focused on the transient stability margin and they either have not carried out the effects of the actuator saturations or they have assumed that all the states of the synchronous machines are available to be measured.…”