Guaranteed cost spacecraft attitude stabilization under actuator misalignments using linear partial differential equations

DOI10.1016/j.jfranklin.2020.03.040zbMath1441.93240OpenAlexW3016114302MaRDI QIDQ776069

Zhong Wang, Yan Li

Publication date: 30 June 2020

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2020.03.040

Mathematics Subject Classification ID

Quadratic programming (90C20) Control/observation systems governed by partial differential equations (93C20) Application models in control theory (93C95) Linear systems in control theory (93C05) Adaptive or robust stabilization (93D21)

Uses Software

• Spinterp
• CVX
• nwSpGr

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