Using a Moving Mass to Change the Spatial Orientation of a Rigid Body Subject to Time-Dependent External Forces

A mechanical system consisting of a rigid body and a material point is considered. They interact with each other by means of internal forces whose physical nature is not defined. Both objects are affected by external forces specified as functions of time. The task is to construct a trajectory for a point mass such that the solid body, under the action of the force of interaction with this mass, changes its orientation in space according to a predetermined program. Based on the theorem on the change in the relative moment of momentum, a second-order vector differential equation, unresolved with respect to the highest derivative, is obtained that describes the system. A change of variables is found that allows replacing the original equation with a first-order vector differential equation resolved with respect to the derivative. All special cases arising from the use of the new equation are considered. The obtained relationships can be used to control spacecraft and robotic systems.

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Publication Details

Journal
Mechanics of Solids
Published
2025-12-01
DOI
https://doi.org/10.1134/s0025654425602198
Primary Topic
Aerospace Engineering and Control Systems
Type
article
Field-Weighted Citation Impact
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article

Using a Moving Mass to Change the Spatial Orientation of a Rigid Body Subject to Time-Dependent External Forces

A. M. Shmatkov
Mechanics of Solids
Aerospace Engineering and Control Systems
article

Using a Moving Mass to Change the Spatial Orientation of a Rigid Body Subject to Time-Dependent External Forces

A. M. Shmatkov
article en

Abstract

A mechanical system consisting of a rigid body and a material point is considered. They interact with each other by means of internal forces whose physical nature is not defined. Both objects are affected by external forces specified as functions of time. The task is to construct a trajectory for a point mass such that the solid body, under the action of the force of interaction with this mass, changes its orientation in space according to a predetermined program. Based on the theorem on the change in the relative moment of momentum, a second-order vector differential equation, unresolved with respect to the highest derivative, is obtained that describes the system. A change of variables is found that allows replacing the original equation with a first-order vector differential equation resolved with respect to the derivative. All special cases arising from the use of the new equation are considered. The obtained relationships can be used to control spacecraft and robotic systems.

Mechanics of SolidsVol. 60(6)
Institute for Problems in Mechanics (RU)
Openalex Percentile: Top 12%
Aerospace Engineering and Control Systems
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