Foucault Pendulum-like problems: A tensorial approach

• Published in: International journal of non-linear mechanics Vol. 43; no. 8; pp. 743 - 760
• Main Authors: Condurache, Daniel, Martinusi, Vladimir
• Format: Journal Article Web Resource
• Language: English
• Published: Elsevier Ltd 01.10.2008; Elsevier
• Subjects: Aerospace & aeronautics engineering; Central force field; Engineering, computing & technology; Foucault Pendulum; Ingénierie aérospatiale; Ingénierie, informatique & technologie; Orthogonal tensors; Relative satellite motion; Rotating reference frame; Vectorial closed form solution; Orthogonal tensors; Foucault Pendulum; Rotating reference frame; Central force field; Vectorial closed form solution; Relative satellite motion; Physical Sciences
• ISSN: 0020-7462; 1878-5638; 1878-5638
• DOI: 10.1016/j.ijnonlinmec.2008.03.009

The paper offers a comprehensive study of the motion in a central force field with respect to a rotating non-inertial reference frame. It is called Foucault Pendulum-like motion and it is a generalization of a classic Theoretical Mechanics problem. A closed form vectorial solution to this famous problem is presented. The vectorial time-explicit solution for the classic Foucault Pendulum problem is obtained as a particular case of the considerations made in the present approach. New interesting conservation laws for the Foucault Pendulum-like motion are deduced by using simple differential and vectorial computations. They help to visualize the shape of the trajectories. Exact vectorial expressions for the law of motion and the velocity are also offered. The case of the driven Foucault Pendulum is also analyzed, and a closed form solution is deduced based on the general considerations. In the end, an new tensorial prime integral for the Foucault Pendulum problem is offered. It helps to reveal in a concise form, within a single entity, all the scalar and vectorial conservation laws for the Foucault Pendulum motion. Two important engineering applications to this approach are presented: the motion of a satellite with respect to a rotating reference frame and the Keplerian relative orbital motion. The latter has a great importance in modeling the problems concerning satellite formation flying, satellite constellations and space terminal rendezvous. The classic problem of the harmonic oscillator in an electromagnetic field is also solved by using the instruments presented in this paper.