Impact-time-control guidance law for missile with time-varying velocity

DOI10.1155/2016/7951923zbMath1400.93056OpenAlexW2466104311WikidataQ59141246 ScholiaQ59141246MaRDI QIDQ1793609

Yanyan Li

Publication date: 12 October 2018

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2016/7951923

Mathematics Subject Classification ID

(H^infty)-control (93B36) Automated systems (robots, etc.) in control theory (93C85) Variable structure systems (93B12) Kinematics of a particle (70B05)

Cites Work

• Designing robust sliding hyperplanes for parametric uncertain systems: A Riccati approach
• Closed-form optimal guidance law for missiles of time-varying velocity
• Analysis and design of integral sliding manifolds for systems with unmatched perturbations

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