In this paper, a linear parameter varying (LPV) modeling and control design approach is
applied to a new class of guided projectiles, aiming to exploit the advantages of the LPV …

In this paper, we develop a reliable Linear Parameter-Varying (LPV) model of the pitch
channel dynamics of a fin-stabilized projectile. Among the available LPV design …

A novel full-envelope controller for an over-actuated fixed-wing vectored thrust eVTOL
aircraft is presented. It proposes a generic control architecture, which is applicable to piloted …

Modern missiles must deal with stringent performance requirements and ensure robustness
across a wide range of operating conditions during flight time. Classic gain-scheduling …

View Video Presentation: https://doi. org/10.2514/6.2023-2498. vid Promising results on LPV
design have been recently proposed, concerning the modeling and control of missiles …

The advent of advanced guidance technologies in the last decades has renewed the interest
in the employment of gun-launched artillery-guided munitions in strategic operations. The …

В обзоре дан анализ докладов 15-го Всемирного конгресса ИФАК, посвященных
теории и системам управления летательными аппаратами. Анализируются также …

We discuss the design of an autopilot for an asymmetric missile. The autopilot is obtained
from controllers designed using H∞ synthesis. Due to important cross-coupling in the pitch …

[3] Pfifer, H.(2012). Quasi-LPV model of a NDI-controlled missile based on function
substitution.[4] Marcos, A. and Balas, GJ (2004). Development of linear-parameter-varying …

Рассматривается канал автоматического управления углом крена летательного
аппарата (ЛА), построенного по самолетной (плоскокрылой) компоновочной схеме …