Closed-Form Solutions for Single-Axis Slew Maneuvers Under a Fixed Final Time Constraint
Author:
Funder
Korea Aerospace University
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-023-00682-5.pdf
Reference24 articles.
1. Byers RM, Vadali SR, Junkins JL (1990) Near-minimum time, closed-loop slewing of flexible spacecraft. J Guid Control Dyn 13:57–65. https://doi.org/10.2514/3.20517
2. Eglynas T, Bogdevicius M, Andziulis A, Jusis M (2017) Trolley motion control based on S-shaped velocity profile for quay crane cargo oscillation comparison. Electron Electr Eng 9:283–288. https://doi.org/10.3846/mla.2017.1034
3. Hecht NK, Junkins JL (1992) Near-minimum-time control of a flexible manipulator. J Guid Control Dyn 15:477–481. https://doi.org/10.2514/3.20860
4. Miu DK, Bhat SP (1991) Minimum power and minimum jerk position control and its applications in computer disk drives. IEEE Trans Magn 27:4471–4475. https://doi.org/10.1109/20.278666
5. Lee D, Bang H (2018) Gimbal-angle vectors of the nonredundant CMG cluster. Int J Aero Space Sci 19:443–458. https://doi.org/10.1007/s42405-018-0037-z
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