This letter concerns trajectory tracking control of attitude dynamics configured on SU(2). Inspired by a popular geometric tracking controller on SO(3), differential geometric tools are used to derive both continuous and discontinuous attitude controllers on the SU(2) manifold, relating these to preexisting controllers operating with imaginary quaternion errors. Additionally, a robustness result is given for the controllers on SU(2), which is illustrated by simulation examples. </p
This work proves that uniform exponential stability is achieved for the attitude control problem by ...
This book consists of two main parts main goal of the first part is to collect and develop new atti...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
This letter concerns trajectory tracking control of attitude dynamics configured on SU(2). Inspired ...
This letter concerns trajectory tracking control of attitude dynamics configured on SU(2). Inspired ...
This paper concerns trajectory tracking control of attitude dynamics configured on SU(2). Inspired b...
This paper addresses three-axis attitude control for a Danish spacecraft, Roemer. The algorithm prop...
This book explores topics that are central to the field of spacecraft attitude determination and con...
The paper adopts the energy shaping method to control of rotational motion. A global representation ...
We present and analyze kinematic-level and dynamic-level feedback control algorithms for single agen...
The objective of this paper is to give a design scheme for attitude control algorithms of a generic ...
This paper studies higher order sliding-modecontrol laws to deal with some spacecraft-attitude-track...
This dissertation presents two major research contributions to the field of attitude dynamics and co...
This paper studies high-order sliding mode control laws to deal with some spacecraft attitude tracki...
This article proposes a novel integral geometric control attitude tracking scheme, utilizing a coord...
This work proves that uniform exponential stability is achieved for the attitude control problem by ...
This book consists of two main parts main goal of the first part is to collect and develop new atti...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
This letter concerns trajectory tracking control of attitude dynamics configured on SU(2). Inspired ...
This letter concerns trajectory tracking control of attitude dynamics configured on SU(2). Inspired ...
This paper concerns trajectory tracking control of attitude dynamics configured on SU(2). Inspired b...
This paper addresses three-axis attitude control for a Danish spacecraft, Roemer. The algorithm prop...
This book explores topics that are central to the field of spacecraft attitude determination and con...
The paper adopts the energy shaping method to control of rotational motion. A global representation ...
We present and analyze kinematic-level and dynamic-level feedback control algorithms for single agen...
The objective of this paper is to give a design scheme for attitude control algorithms of a generic ...
This paper studies higher order sliding-modecontrol laws to deal with some spacecraft-attitude-track...
This dissertation presents two major research contributions to the field of attitude dynamics and co...
This paper studies high-order sliding mode control laws to deal with some spacecraft attitude tracki...
This article proposes a novel integral geometric control attitude tracking scheme, utilizing a coord...
This work proves that uniform exponential stability is achieved for the attitude control problem by ...
This book consists of two main parts main goal of the first part is to collect and develop new atti...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...