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Title
Authors
Inertial Navigation in Space Using the Regular Quaternion Equations of Astrodynamics
Chelnokov Y.N.
Optimal Control of a Spacecraft Orientation Taking into Account the Energy of Rotation
Levskii M.V.
Optimal Control of Kinetic Moment During the Spatial Rotation of a Rigid Body (Spacecraft)
Levskii M.V.
Pulsed Optimal Spacecraft Orbit Reorientation by Means of Reactive Thrust Orthogonal to the Osculating Orbit. II
Sapunkov Y.G., Chelnokov Y.N.
Quaternion Regularization of the Equations of the Perturbed Spatial Restricted Three-Body Problem: II
Chelnokov Y.N.
Pulsed Optimal Spacecraft Orbit Reorientation by Means of Reactive Thrust Orthogonal to the Osculating Orbit. I
Sapunkov Y.G., Chelnokov Y.N.
An Analytical Solution to the Problem of Optimal Control of the Reorientation of a Rigid Body (Spacecraft) Using Quaternions
Levskii M.V.
Quaternion Regularization of the Equations of the Perturbed Spatial Restricted Three-Body Problem: I
Chelnokov Y.N.
Quaternion Solution of the Problem of Optimal Rotation of the Orbit Plane of a Variable-Mass Spacecraft Using Thrust Orthogonal to the Orbit Plane
Sapunkov Y.G., Chelnokov Y.N.
Kinematic problem of optimal nonlinear stabilization of angular motion of a rigid body
Biryukov V.G., Chelnokov Y.N.
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