Control variable parameterisation with penalty approach for hypersonic vehicle reentry optimisation

DOI10.1080/00207179.2018.1426882zbMath1421.93098OpenAlexW2784234514MaRDI QIDQ5231422

Ping Wang, Zhang Ren, Ping Liu, Jie Yan, Xinggao Liu, Long Xiao, Guodong Li

Publication date: 27 August 2019

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207179.2018.1426882

zbMATH Keywords

penalty methodhypersonic flight vehiclecontrol variable parameterisationreentry optimisationsmooth technology

Mathematics Subject Classification ID

Nonlinear programming (90C30) Quadratic programming (90C20) Application models in control theory (93C95) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (3)

On flexibility of constraints system under approximation of optimal control problems ⋮ Adaptive control arc length-based time grid refinement control parameterisation method for unmanned hypersonic vehicle reentry trajectory optimisation ⋮ A limited-memory BFGS-based differential evolution algorithm for optimal control of nonlinear systems with mixed control variables and probability constraints

Uses Software

• SOCS

Cites Work

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