Back
ExamFull examExam paper only

09 09 14

Full exam for Dynamics and Control of Space Structures in the Aerospace Engineering degree programme at Politecnico di Milano. The document covers: ID codes: 072652 SPA 2 liv, 081225 SPA Mag, 091932 SPA Mag Date: 09 September 2014 Instructor: Lorenzo Dozio 1. The system in Figure 1 consists of a rigid hub with a cantilever flexible appendage carrying a tip payload. The hub is modeled as a rigid disk hinged at its center,

Dynamics and Control of Space StructuresFull exam

Document information

What's included in this study material

Full exam for Dynamics and Control of Space Structures in the Aerospace Engineering degree programme at Politecnico di Milano. The document covers: ID codes: 072652 SPA 2 liv, 081225 SPA Mag, 091932 SPA Mag Date: 09 September 2014 Instructor: Lorenzo Dozio 1. The system in Figure 1 consists of a rigid hub with a cantilever flexible appendage carrying a tip payload. The hub is modeled as a rigid disk hinged at its center,

Import quality: text was extracted directly from the original document.

Extracted content from the document

Representative passages recognised in different parts of the material. The full extracted text remains available to search, while this compact preview makes the page easier to read.

Page 1

ID codes: 072652 SPA 2 liv, 081225 SPA Mag, 091932 SPA Mag Date: 09 September 2014 Instructor: Lorenzo Dozio 1. The system in Figure 1 consists of a rigid hub with a cantilever flexible appendage carrying a tip payload. The hub is modeled as a rigid disk hinged at its center, with radius R and moment of inertia Ih. The appendage is modeled as a homogeneous slender beam of length ℓ, mass per unit length m and flexural stiffness EJ . The payload is modeled as a mass mt and inertia It. A prescribed torque Mc acts on the hub. x y X Y R, I h EJ, m, ℓ mt, I t Mc θ w Figure 1: Dynamic system of problem 1 (a) Write the exact linearized differential problem governing the planar dynamics of the s ystem (equations of motion and boundary conditions) in terms of rotation angle θ(t) and transverse deflection w(x, t ) of the flexible appendage. Assume small rotation speed ˙θ and small w. (b) Write the approximate equations of motion of the system according to an appropriate Ritz -Galerkin discretization and explain how to compute the bending moment along t he flexible appendage using the mode acceleration method. 2. The system in Figure 2 consists of a rigid body of mass M and moment of inertia J with respect to the center of mass (CM). The body is supported by two massless rods of length ℓ and damping coefficient β proportional to the stiffness. The sys- tem is forced by a prescribed base displacement w. Write the time-domain equations to compute the variance of the relative displacement z = v − w of CM when the base acceleration is a white noise of intensity W . w(t) v(t) EA, ℓ, β 2EA, ℓ, β M, J L1 L2 CM Figure 2: Dynamic system of problem 2 3. Let’s consider a LTI system ˙ z(t) = az(t) + bu(t), where the control variable u is actually provided by an actuator having an internal dynamics with…

Preview

First page of the document.

First page: 09 09 14