By equating moments about the c. of g. the differential equation that models the satellite is: d²0 dt² J- = d.F where is the output angle, F is the input force, d is the distance the thrusters are from the c. of g. and J is the moment of inertia. By taking Laplace Transforms of both sides determine a transfer function, G(s), where e is the output and F is the input. Enter the transfer function into Matlab and use the LTIview facility to plot a time response to a unit step input assuming the satellite is initially stationary.

By equating moments about the c. of g. the differential equation that models the satellite is: d²0 dt² J- = d.F where is the output angle, F is the input force, d is the distance the thrusters are from the c. of g. and J is the moment of inertia. By taking Laplace Transforms of both sides determine a transfer function, G(s), where e is the output and F is the input. Enter the transfer function into Matlab and use the LTIview facility to plot a time response to a unit step input assuming the satellite is initially stationary.

Introductory Circuit Analysis (13th Edition)

13th Edition

ISBN:9780133923605

Author:Robert L. Boylestad

Publisher:Robert L. Boylestad

Chapter1: Introduction

Section: Chapter Questions

Problem 1P: Visit your local library (at school or home) and describe the extent to which it provides literature...

See similar textbooks

Similar questions

Use Routh-Hurwitz method, how many roots are on the left-half plane by the polynomial equation 3 0 2 4
Solve by Laplace transform
Given the vector: A=[–4.2, 3.5. –2.2]. Which is the cross product D = AxA ?
For the following mechanical systems, obtain the equations of motion in Laplace domain.
Question (1) a. Consider F(z) 0.5 z-1 find f(k) using the partial fraction method 0.62-2-1.62-1+1.0
S= 12a_r + 5a_0 + Tia_Q and T = 2a_r+ 0.5rta_e are two vectors at point (2,1,T/2) and (5,TL/2,1/2), respectively. Determine the angle between S and T.
Determine the system function, H(z) of the difference equation given:y(n) = 0.9571y(n-1) - 0.4268y(n-2) + 0.0625y(n-3) + 0.3273x(n) - 0.3273x(n-2)
Please reduce using trigonometric identities and complex numbers to the format provided.
Q2. For each of the following z-transforms, determine the inverse: (a) Ya(z) = (1- z) (1 – 2z-1)(1 – 3z) with ROC: 0 1. (c) Y.(z) = with ROC defined to get a two-sided signal y[n]. (6-5z-1+z-:
D is a viscous damper, 10N-m/rad