2015
DOI: 10.1109/taes.2015.140219
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OQTAL: Optimal quaternion tracking using attitude error linearization

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Cited by 17 publications
(8 citation statements)
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“…Ensuring that that Ω and ϑ asymptotically converge to zero and following (1), then q → q O . Expanding the components of every axis from (21), it yields (13), (14) and (15).…”
Section: A Attitude Control Formulationmentioning
confidence: 99%
See 1 more Smart Citation
“…Ensuring that that Ω and ϑ asymptotically converge to zero and following (1), then q → q O . Expanding the components of every axis from (21), it yields (13), (14) and (15).…”
Section: A Attitude Control Formulationmentioning
confidence: 99%
“…[16] designed a robust quaternion-based sliding mode algorithm for tracking attitude spacecraft trajectories. [14] and [13] proposed optimal control techniques for quadrotors based on quaternion attitude error equations. Some of the first works that have combined sliding mode theory with quaternionbased models were [5], [27] and [4], where attitude sliding mode controllers based on the kinematic quaternion equations of a general rigid aircraft were introduced.…”
Section: Introductionmentioning
confidence: 99%
“…Several other papers, as (Wie & Barba, 1985) and (Ghiglino, Forshaw, & Lappas, 2015), utilize the quaternion representation to develop their control strategy discussing, respectively, stability related results for large angle maneuvers, derived from Lyapunov's theory, and optimal LQR-based control results. Regarding stability, a significant contribution was given by (Wen & Kreutz-Delgado, 1991), discussing the global properties of several control laws for quaternion represented attitude problems.…”
Section: Review and Paper Contributionmentioning
confidence: 99%
“…O bviously, the Space Manoeuvre Vehicles (SMV) is going to play an increasingly important role in future exploration of space. Therefore, a well-designed trajectory, particularly in the skip entry phase, is key to the stable flight and improved guidance control of the vehicle [1]- [4]. Unlike traditional mission profiles discussed in [5]- [8], the mission scenario investigated in this paper focuses on the atmospheric skip hopping, targeting the entry into the atmosphere down to a predetermined position (predetermined altitude given by the industrial sponsor of this project) and the required controls involved in returning back to the orbit.…”
Section: Introductionmentioning
confidence: 99%