IEEE - Institute of Electrical and Electronics Engineers, Inc. - Anti-unwinding Attitude Control of Spacecraft using Back-Stepping Technique with Finite Time Convergence

2018 15th International Conference on Control, Automation, Robotics and Vision (ICARCV)

Author(s): Umair Javaid
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 November 2018
Conference Location: Singapore, Singapore, Singapore
Conference Date: 18 November 2018
Page(s): 692 - 697
ISBN (Electronic): 978-1-5386-9582-1
ISBN (USB): 978-1-5386-9581-4
DOI: 10.1109/ICARCV.2018.8581317
Regular:

Quaternion representation of spacecraft has double equilibrium points associated with it, which may cause unwinding phenomenon in attitude control if both equilibria are not treated as stable... View More

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