2013
DOI: 10.1007/s10409-013-0067-5
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Attitude control of a rigid spacecraft with one variable-speed control moment gyro

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Cited by 11 publications
(3 citation statements)
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“…19 The GDI control design methodology has been applied to several aerospace control engineering problems. 17,18,[20][21][22][23] The GDI control methodology is rooted in analytical mechanics, and it was inspired by the Udwadia-Kalaba equations of motion. 24 It allows for two cooperating controllers that act on two orthogonally complement control spaces: one is the particular controller that realizes the dynamic constraints, and the other is the auxiliary controller that is affine in the null control vector, and is utilized in this article to enforce global inner closed-loop stability.…”
Section: Introductionmentioning
confidence: 99%
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“…19 The GDI control design methodology has been applied to several aerospace control engineering problems. 17,18,[20][21][22][23] The GDI control methodology is rooted in analytical mechanics, and it was inspired by the Udwadia-Kalaba equations of motion. 24 It allows for two cooperating controllers that act on two orthogonally complement control spaces: one is the particular controller that realizes the dynamic constraints, and the other is the auxiliary controller that is affine in the null control vector, and is utilized in this article to enforce global inner closed-loop stability.…”
Section: Introductionmentioning
confidence: 99%
“…19 The GDI control design methodology has been applied to several aerospace control engineering problems. 17,18,2023…”
Section: Introductionmentioning
confidence: 99%
“…By virtue of this design, the simplifying tactics that are often essential to derive the inverse dynamics in classical DI were relaxed. This control design technique has been an effective tool for several aerospace engineering control applications (Bajodah, 2009a; Bajodah, 2009b; Hall et al , 2010; Bajodah, 2010; Hameduddin and Bajodah, 2012; Gui et al , 2013a, 2013b).…”
Section: Introductionmentioning
confidence: 99%