Add to ORKGVariational equations were applied to the case of a rapidly spinning triaxial body moving in an elliptic orbit, in which the orbital plane is regressing at a constant rate. The explicit differential equations obtained in this application were integrated by the method of averaging to develop secular analytical expressions, which, to first-order in a small parameter, describe the complete space motions of the rigid body under the influence of nonresonant gravity-gradient perturbations. The effects of aerodynamic torque on the rotational motion of an orbiting satellite are studied, as another example of the application of the variational equations derived and the method of averaging
The equations for the variations of the Keplerian elements of the orbit of a spacecraft perturbed by...
A higher-order perturbation theory for the rotation of a uniaxial satellite under gravity-gradient t...
peer reviewedIn this presentation we revisit the analytical determination of the corotation solution...
The second and final step in the development of first-order secular solutions to rotational motions ...
Averaging technique applied to variational equations describing rotational motions of rigid triaxial...
In his paper I examine influence of small gravitational torque on rotation of elongated triaxial bod...
Perturbed rotations of a rigid body close to the Lagrange case under the action of perturbation torq...
Celestial mechanics perturbation methods applied to problem of describing motion of rigid artificial...
Orbital motion effects from attraction by rotating source with numerical solution
The book presents a unified and well-developed approach to the dynamics of angular motions of rigid ...
Abstract: A spinning mode is analyzed for orientation of an Earth low orbit artificial sat...
Dynamical Systems Theory (DST) serves as a means to understand and describe the changes that occur o...
International audienceIn this paper we discuss the influence of the triaxiality of a celestial body ...
The Lagrange’s planetary equations written in terms of the classical orbital elements have the disad...
Linearized perturbation theory for calculating relative motion of unrestrained bodies within orbitin...
The equations for the variations of the Keplerian elements of the orbit of a spacecraft perturbed by...
A higher-order perturbation theory for the rotation of a uniaxial satellite under gravity-gradient t...
peer reviewedIn this presentation we revisit the analytical determination of the corotation solution...
The second and final step in the development of first-order secular solutions to rotational motions ...
Averaging technique applied to variational equations describing rotational motions of rigid triaxial...
In his paper I examine influence of small gravitational torque on rotation of elongated triaxial bod...
Perturbed rotations of a rigid body close to the Lagrange case under the action of perturbation torq...
Celestial mechanics perturbation methods applied to problem of describing motion of rigid artificial...
Orbital motion effects from attraction by rotating source with numerical solution
The book presents a unified and well-developed approach to the dynamics of angular motions of rigid ...
Abstract: A spinning mode is analyzed for orientation of an Earth low orbit artificial sat...
Dynamical Systems Theory (DST) serves as a means to understand and describe the changes that occur o...
International audienceIn this paper we discuss the influence of the triaxiality of a celestial body ...
The Lagrange’s planetary equations written in terms of the classical orbital elements have the disad...
Linearized perturbation theory for calculating relative motion of unrestrained bodies within orbitin...
The equations for the variations of the Keplerian elements of the orbit of a spacecraft perturbed by...
A higher-order perturbation theory for the rotation of a uniaxial satellite under gravity-gradient t...
peer reviewedIn this presentation we revisit the analytical determination of the corotation solution...