A study is made of a controllable mechanical system in the form of a Timoshenko beam with a weight. The system models a flexible-link robot manipulator. A Galerkin approximation based on the solutions of the corresponding Sturm-Liouville problem is constructed for the partial differential equations of motion. Conditions of local controllability of the Galerkin approximation in the neighborhood of the system's equilibrium state are established. The stabilizability of the equilibrium state is proved, and an explicit scheme for feedback control design is proposed Keywords: controllable mechanical system, Timoshenko beam, flexible-link robot manipulator, Galerkin approximation, local controllability condition, stabilizability of equilibrium state, explicit scheme for feedback control designIssues of dynamics and control of flexible-link robot manipulators are addressed in the monographs [5, 15, 16] and papers [9,10,19]. The equations of spatial motion of a linkage described by the Euler-Bernoulli and Timoshenko beam models are derived in [1]. The stabilization of a controllable system with two Euler-Bernoulli beams is studied in [2].Control problems for the Timoshenko beam are analyzed in [8,11,13,14,17,18]. However, these papers considered free-end beams and disregarded the gravity. In the present paper, we analyze the dynamic equations of a Timoshenko beam connected with a rigid body. Such a model describes the motion of a controllable manipulator in the gravity field.1. Model Description. Consider a flexible beam (a flexible-link manipulator) rotating about a fixed point O (Fig. 1). Let a weight of mass m be attached to the free end O 1 of the beam and a control moment M act on the beam at the point O. Denote the length of the beam by l. The configuration of the mechanical system at time t ≥ 0 is defined by functions ϕ(t), w(x, t), and ψ (x, t) (0 ≤ x ≤ l), where ϕ(t) is the angle between the moving axis Ox and the horizontal direction, w (x, t) is the deflection of the beam's central line at a point with abscissa x ∈ [0, l], and ψ (x, t) is the angular deflection of the beam.The mass distribution in the weight is characterized by a moment of inertia J c about its center of mass C. Denote by ψ c the angle between the vector O 1 C and the normal vector to the cross section of the beam at x = l.Following the Timoshenko beam model [3], we write the Lagrangian of the mechanical system: 2 2 2 2 2 2 2