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IssuesArchive of Issues2002-1pp.138-148

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A. V. Petrovskii, "Stability and post-critical behavior of an inverted 3D pendulum under non-potential loading," Mech. Solids. 37 (1), 138-148 (2002)
Year 2002 Volume 37 Number 1 Pages 138-148
Title Stability and post-critical behavior of an inverted 3D pendulum under non-potential loading
Author(s) A. V. Petrovskii (Moscow)
Abstract We consider an inverted pendulum with visco-elastic gimbals between the links and study its behavior under dead loads and follower forces. The stability of its states of equilibrium is analyzed with respect to the control parameters (dead load and follower force). The post-critical behavior of the pendulum is studied, in particular, the stability of its periodic motion in the plane of its initial stability loss.

The behavior of elastic systems subjected to non-potential forces (in particular, follower forces) has been thoroughly studied in [1-6]. However in this field, there still remain many problems that are of interest in the context of the nonlinear dynamics. In this respect, an interesting and characteristic problem is that of the behavior of an inverted pendulum subjected to a dead load and a follower force. For instance, a pendulum may possess two mutually orthogonal principal planes of rigidity and damping. The instability of such a pendulum occurs in one of these planes. In this problem, apart from the usual factors (non-potentiality of loads and damping) considered in the studies of the post-critical behavior of systems, it is important to take into account the interaction of the vibration modes in the two principal planes. Moreover, it is interesting to analyze a combination of quasi-static (divergence) and dynamic (flutter) types of instability. In this case, secondary flutter may arise in the divergence region. This phenomenon was discovered in aero-elastic systems [7] and was later studied in detail in [8-10].

The present paper offers a systematic analysis of equilibrium states of divergence type for an inverted 3D double pendulum, as well as an investigation of its motions in the flutter region. The main attention is given to the stability of these states. Just as is the case for aero-elastic systems, the phenomenon of secondary flutter occurs in the divergence domain. In contrast to aero-elastic systems, where this phenomenon is observed only if certain relations between partial damping parameters are satisfied, the secondary flutter always takes place in the pendulum case.
References
1.  V. V. Bolotin, "On vibrations and stability of rods subjected to non-conservative forces," in Turbine Installations [in Russian], pp. 23-42, Izd-vo AN SSSR, Moscow, 1959.
2.  V. V. Bolotin, Non-conservartive Problems in the Theory of Elastic Stability [in Russian], Fizmatgiz, Moscow, 1961.
3.  V. V. Bolotin and N. I. Zhinzher, "Effects of damping on the stability of elastic systems subjected to non-conservative forces," Int. J. Solid. and Struct., Vol. 5, No. 9, pp. 965-989, 1969.
4.  N. I. Zhinzher, "Effect of dissipative forces with incomplete dissipation on the stability of elastic systems," Izv. AN. MTT [Mechanics of Solids], No. 1, pp. 149-155, 1994.
5.  J.-D Jin, "Bifurcation analysis of double pendulum with a follower force," J. Sound. Vibrat., Vol. 154, No. 2, pp. 191-204, 1992.
6.  A. N. Kounadis, "On the failure of static stability analysis of nonconservative systems in regions of divergence instability," Intern. J. Solids and Struct., Vol. 31, No. 15, pp. 2099-2120, 1994.
7.  V.V. Bolotin, A. V. Petrovskii, and A. A. Grishko, "Secondary bifurcations and global instability of an aeroelastic nonlinear system in the divergence domain," J. Sound and Vibrat., Vol. 191, No. 3, pp. 431-451, 1996.
8.  A. A. Grishko, A. V. Petrovskii, and V. P. Radin, "The effect of internal friction on the stability of a panel in supersonic gas flow," Izv. AN. MTT [Mechanics of Solids], No. 1, pp. 173-181, 1998.
9.  V. V. Bolotin, A. A. Grishko, A. N. Kounadis, and Ch. Gantes, "Nonlinear panel flutter in remote post-critical domain," Intern. J. Nonlin. Mech., Vol. 33, No. 5, pp. 753-764, 1998.
10.  V. V. Bolotin, A. A. Grishko, A. N. Kounadis, Ch. Gantes, and J. B. Roberts, "Influence of initial conditions on the post-critical behavior of nonlinear aeroelastic system," J. Nonlin. Dynamics, Vol. 15, No. 1, pp. 63-81, 1998.
11.  V. V. Bolotin (Editor), Vibrations in Technology. Handbook. Volume 1. Vibrations of Linear Systems [in Russian], Mashinostroenie, Moscow, 1999.
12.  A. A. Grishko, Yu. A. Dubrovskikh, and A. V. Petrovskii, "On the post-critical behavior of dissipative nonlinear systems," Prikl. Mekh., Vol. 34, No. 6, pp. 92-98, 1998.
Received 06 December 1999
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