Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable Rockets

What is it about?

We present a unified strategy for trajectory-attitude control of reusable rockets during the aerodynamic descent phase of the flight. The control strategy is based on the use of structured robust control. After deriving the full state-space representation for the rocket we analyze the behavior of the closed-loop system with linear and nonlinear methodologies.

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