In this paper, we propose a novel framework that provides a systematic strategy to regulate the rigid body attitude on SO(3) within a generic constrained attitude zone. The proposed control scheme consists of three components: sampling, planning and low-level control. Specifically, an overlapping cell-like sampling for the attitude configuration space SO(3) is built and further reformulated to a graph model. Based on this abstraction, a complete graph search algorithm is utilized to generate a feasible path in the graph model. Both sufficient and necessary conditions on finding a feasible path are presented. Furthermore, to facilitate the control design, the point-to-point path is transformed into a smooth reference trajectory along the geo...
This article presents a semianalytical method for motion planning with pointing and dynamic constrai...
The purpose of the present work is to perform spacecraft attitude motion planning so that a rest-to-...
A motion planning technique for generating smooth attitude slew maneuvers is presented, which can ge...
In this paper, we propose a novel framework that provides a systematic strategy to regulate the rigi...
A method for spacecraft attitude motion planning presented in [Celani and Lucarelli, 2019] is applie...
Thesis (Ph.D.)--University of Washington, 2013The main research in this dissertation deals with tran...
Constrained attitude maneuvers have numerous applications in robotics and aerospace. In our previous...
The collocation method is extended to the special orthogonal group SO(3) with application to optimal...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
The purpose of the present work is to perform spacecraft attitude motion planning using a method des...
We develop nonlinear reference governor and nonlinear model predictive control schemes for constrain...
textTo satisfy the requirements of small satellites with attitude control requirements, a guidance, ...
This dissertation explores aspects of control in rigid-body and robotic systems. The first and secon...
The purpose of the present work is to perform spacecraft attitude motion planning so that a rest-to ...
The Satellite Design Laboratory at the University of Texas at Austin is building a general purpose g...
This article presents a semianalytical method for motion planning with pointing and dynamic constrai...
The purpose of the present work is to perform spacecraft attitude motion planning so that a rest-to-...
A motion planning technique for generating smooth attitude slew maneuvers is presented, which can ge...
In this paper, we propose a novel framework that provides a systematic strategy to regulate the rigi...
A method for spacecraft attitude motion planning presented in [Celani and Lucarelli, 2019] is applie...
Thesis (Ph.D.)--University of Washington, 2013The main research in this dissertation deals with tran...
Constrained attitude maneuvers have numerous applications in robotics and aerospace. In our previous...
The collocation method is extended to the special orthogonal group SO(3) with application to optimal...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
The purpose of the present work is to perform spacecraft attitude motion planning using a method des...
We develop nonlinear reference governor and nonlinear model predictive control schemes for constrain...
textTo satisfy the requirements of small satellites with attitude control requirements, a guidance, ...
This dissertation explores aspects of control in rigid-body and robotic systems. The first and secon...
The purpose of the present work is to perform spacecraft attitude motion planning so that a rest-to ...
The Satellite Design Laboratory at the University of Texas at Austin is building a general purpose g...
This article presents a semianalytical method for motion planning with pointing and dynamic constrai...
The purpose of the present work is to perform spacecraft attitude motion planning so that a rest-to-...
A motion planning technique for generating smooth attitude slew maneuvers is presented, which can ge...