Improved guidance algorithm considering terminal attitude constraints for spacecrafts via optimal control theory

DOI10.1002/oca.2588zbMath1469.93085OpenAlexW3008218151MaRDI QIDQ5003567

Baogang Lu, Changzhu Wei, Yu'an Li

Publication date: 22 July 2021

Published in: Optimal Control Applications and Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/oca.2588

zbMATH Keywords

optimal controlnumerical methodspacecraftsterminal attitude constraint

Mathematics Subject Classification ID

Control/observation systems governed by partial differential equations (93C20) Application models in control theory (93C95) Existence theories for optimal control problems involving partial differential equations (49J20)

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