Dual-loop finite-time sliding mode control for six-DOF plane-symmetric launch vehicle during large-angle maneuvers

ZHENG Zixin; ZHANG Fei; QI Ruiyun; HU Cunming

doi:10.13700/j.bh.1001-5965.2025.0787

Article Contents

Journal of Beijing University of Aeronautics and Astronautics > 2026 > Accepted Manuscript

ZHENG Zixin, ZHANG Fei, QI Ruiyun, et al. Dual-loop finite-time sliding mode control for six-DOF plane-symmetric launch vehicle during large-angle maneuvers[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0787(in Chinese)

Citation:

ZHENG Zixin, ZHANG Fei, QI Ruiyun, et al. Dual-loop finite-time sliding mode control for six-DOF plane-symmetric launch vehicle during large-angle maneuvers[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0787(in Chinese)