1995
DOI: 10.1016/s1474-6670(17)46878-9
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Control on the Sphere and Reduced Attitude Stabilization

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Cited by 78 publications
(91 citation statements)
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“…Almost global reduced attitude stabilizing controllers on S 2 have been studied in [4], [8], [9], [10], [11]. In [4], [8] a control system that stabilizes a rigid body to a fixed reference direction q d ∈S 2 is summarized, where the error function used in [8] is,…”
Section: A Error Functionmentioning
confidence: 99%
“…Almost global reduced attitude stabilizing controllers on S 2 have been studied in [4], [8], [9], [10], [11]. In [4], [8] a control system that stabilizes a rigid body to a fixed reference direction q d ∈S 2 is summarized, where the error function used in [8] is,…”
Section: A Error Functionmentioning
confidence: 99%
“…Stemming from the seminal work of [1] about control theory on general Lie groups, much of the literature has been devoted to the control of systems defined on SO(3) and SE (3). Although it is usual to design controllers for these systems using matrices to represent elements of these Lie groups [2], [3], it has been noted by some authors that controllers designed using another type of representation, namely, the unit quaternions for SO (3) and the unit dual quaternions for SE (3), may have advantages regarding computational time and storage requirements [4], [5].…”
Section: Introductionmentioning
confidence: 99%
“…This work is a contribution in the area of nonlinear control theory for mechanical systems (Murray 1995) and it is the completion of our previous works and (Bullo, Murray and Sarti 1995). Given a fully actuated control system, that is a system with as many inputs as degrees of freedom, our control objective is to track a trajectory with exponential convergence rates and to guarantee performance and robustness.…”
Section: Introductionmentioning
confidence: 99%