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A satellite controls its rotational velocity by extending an arm much like a balle- rina in a spin or a figure skater. Changing the length, L, of the arm changes the inertia of the satellite. The transfer function between the rotational velocity, w(s), and the incremental change in L, called AL(s) is given as w(s) AL(s) 2(s+4) (s +5) (s + 1)² The change in length is given as 1 AL(s) == S (4) (5) Determine the response to the change in length of the satellite's angular veloc- ity, w(t), in the time domain using partial fractions.

A satellite controls its rotational velocity by extending an arm much like a balle- rina in a spin or a figure skater. Changing the length, L, of the arm changes the inertia of the satellite. The transfer function between the rotational velocity, w(s), and the incremental change in L, called AL(s) is given as w(s) AL(s) 2(s+4) (s +5) (s + 1)² The change in length is given as 1 AL(s) == S (4) (5) Determine the response to the change in length of the satellite's angular veloc- ity, w(t), in the time domain using partial fractions.

Introductory Circuit Analysis (13th Edition)
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...
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A satellite controls its rotational velocity by extending an arm much like a balle- rina in a spin or a figure skater. Changing the length, L, of the arm changes the inertia of the satellite. The transfer function between the rotational velocity, w(s), and the incremental change in L, called AL(s) is given as w(s) AL(s) 2(s+4) (s +5) (s + 1)² The change in length is given as 1 AL(s) == S (4) (5) Determine the response to the change in length of the satellite's angular veloc- ity, w(t), in the time domain using partial fractions.
Transcribed Image Text:A satellite controls its rotational velocity by extending an arm much like a balle- rina in a spin or a figure skater. Changing the length, L, of the arm changes the inertia of the satellite. The transfer function between the rotational velocity, w(s), and the incremental change in L, called AL(s) is given as w(s) AL(s) 2(s+4) (s +5) (s + 1)² The change in length is given as 1 AL(s) == S (4) (5) Determine the response to the change in length of the satellite's angular veloc- ity, w(t), in the time domain using partial fractions.
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