Robust fixed structure output feedback flight control law synthesis and analysis using singular structured value

Author:

Siqueira Daniel,Paglione Pedro,Moreira Fernando J.O.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

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1. Autopilot Structured H∞ Synthesis for Satisfying Gain and Phase Margin Constraints;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2019-04

2. Linear near-equilibrium glide model for unpowered entry trajectory control;Aerospace Science and Technology;2017-11

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