The paper presents an exact, analytical solution for the planar attitude dynamics of a rigid body, located at an equilibrium point of the Circular Restricted Three-Body Problem. The dynamics equations are proved to be analogous to the nonlinear dynamics of a swinging pendulum, for which exact solution exists in literature, and is thus applied to the present case. Three-dimensional attitude stability of the rotating body is investigated, both for oscillations (no net swing over) and for multiple swings, extending the literature results on the topic. Eventually, three-dimensional periodic solutions are presented and analyzed
The development of multi-joint-spacecraft mission concepts calls for a deeper understanding of their...
The three-dimensional, nonlinear, coupled orbit and attitude motion of a spacecraft in both planar a...
The development of analytic solutions for the forced attitude motion of a rigid body is a formidable...
The paper presents an exact, analytical solution for the planar attitude dynamics of a rigid body, l...
The paper presents an exact, analytical solution for the planar attitude dynamics of a rigid body, l...
The paper presents an exact, analytical solution for the planar attitude dynamics of a rigid body, l...
Attitude control is fundamental to the design and operation of many large engineering systems that c...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
Abstract: A rigid base body, supported by a fixed pivot point, is free to rotate in three dimensions...
In this paper, a solution to the problem of rest-to-rest three-axis attitude reorientation of a full...
In this paper, a solution to the problem of rest-to-rest three-axis attitude reorientation of a full...
Abstract--For p oblems involving rotating rigid bodies (e.g. spin-stabilized satellites inspace) one...
The development of multi-joint-spacecraft mission concepts calls for a deeper understanding of their...
The three-dimensional, nonlinear, coupled orbit and attitude motion of a spacecraft in both planar a...
The development of analytic solutions for the forced attitude motion of a rigid body is a formidable...
The paper presents an exact, analytical solution for the planar attitude dynamics of a rigid body, l...
The paper presents an exact, analytical solution for the planar attitude dynamics of a rigid body, l...
The paper presents an exact, analytical solution for the planar attitude dynamics of a rigid body, l...
Attitude control is fundamental to the design and operation of many large engineering systems that c...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
The attitude motion of a rigid spacecraft in fully nonlinear reference orbits is explored in this in...
Abstract: A rigid base body, supported by a fixed pivot point, is free to rotate in three dimensions...
In this paper, a solution to the problem of rest-to-rest three-axis attitude reorientation of a full...
In this paper, a solution to the problem of rest-to-rest three-axis attitude reorientation of a full...
Abstract--For p oblems involving rotating rigid bodies (e.g. spin-stabilized satellites inspace) one...
The development of multi-joint-spacecraft mission concepts calls for a deeper understanding of their...
The three-dimensional, nonlinear, coupled orbit and attitude motion of a spacecraft in both planar a...
The development of analytic solutions for the forced attitude motion of a rigid body is a formidable...