This paper studies the mechanics of reusable retropropelled flight of slender low lift-to-drag
bodies via integrated guidance and control simulations. To do this, a simulation benchmark …

This paper investigates the use of structured robust techniques for the control design of the
aerodynamic descent phase of a reusable rocket. A unified control strategy based on the …

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 …

View Video Presentation: https://doi. org/10.2514/6.2023-2171. vid Rocket reusability is a
key-factor for a sustainable and cost-effective future of space missions. Despite successes in …

This paper presents a new application of structured H∞ synthesis to tune self-scheduled
controllers. Newly available MATLAB-based tools allow to tune fixed-structure linear …

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 …

This paper investigates the use of structured H∞ control for the aerodynamic descent phase
of a reusable rocket. A unified control strategy for attitude and position is proposed and …

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 …

In this paper, the feasibility of structured H∞ control design is demonstrated in
representative environment for flexible launcher control during non-stationary ascent phase …