This paper discusses the problem of synthesizing robust controllers for reusable
rocketsduring the aerodynamic descent phase. Emphasis is given to a well-established …

This paper presents a systematic robust control framework based on the structured
approach to address the synthesis of the atmospheric ascent‐flight control system of a …

This paper presents a new procedure for the integrated plant and flight control system
design in the presence of parametric uncertainties. The proposed approach is based on a …

This article describes the application of two robust control design techniques: the structured
H-infinity and the linear parameter varying (LPV) synthesis techniques to the design of the …

This article presents the design of an atmospheric control system for the VEGA launcher
using Linear Parameter-Varying (LPV) synthesis techniques, both non-rate and rate …

IN SPITE of recent advances in control system theory, gain-scheduling techniques remain a
viable approach for the control of a great variety of nonlinear systems [1, 2] and are widely …

This paper studies the synthesis of a robust control system via structured H∞ for the full
atmospheric re-entry problem of Reusable Launch Vehicles (RLVs). This control system is …

This article describes a methodology for structured H-infinity synthesis that reconciles
classical and robust control concepts. The aim is to provide a transparent and …

In this article, a complete modelling, synthesis, and analysis methodology of control
compensators for descent and landing (D&L) on small planetary bodies is presented. These …

This article addresses the design of the atmospheric ascent-flight control system of a launch
vehicle using the structured H∞ synthesis technique. The main goal is to provide a …