Missile Autopilot Design via Structured Robust Linear Parameter-Varying Synthesis-Reference-Cited by-同舟云学术

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Missile Autopilot Design via Structured Robust Linear Parameter-Varying Synthesis

Published:2023-08 Issue:8 Volume:46 Page:1649-1656
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Simões Alberto M.¹^ORCID,Cavalcanti Vinícius M. G. B.¹^ORCID

Affiliation:

1. Military Institute of Engineering, 22290-270 Rio de Janeiro, Brazil

Funder

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G007580

Reference25 articles.

1. Dynamic scheduling of modern-robust-control autopilot designs for missiles

2. Gain scheduling for H-infinity controllers: a flight control example

3. Missile Autopilot Design: Gain-Scheduling and the Gap Metric

4. Smoothly Gain-Scheduled Control of a Tri-Turbofan Airship

5. Gain-Scheduling Control Design in the Presence of Hidden Coupling Terms

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