Electrical Motor Controls for Integrated Systems
5th Edition
ISBN: 9780826912268
Author: Gary Rockis;Glen A. Mazur
Publisher: American Technical Publishers
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Chapter 1.3, Problem 4CP
To determine
The unit for the inductive and capacitive reactances.
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A communication satellite is in stationary (synchronous) orbit about the earch (assume
altitude of 22.300 statute miles). Its transmitter generates 8.00 W. Assume the transmit-
ting antenna is isotropic. Its signal is received by the 210-ft diameter tracking parabo-
loidal antenna on the earth at the NASA tracking station at Goldstone, California. Also
assume no resistive loss in either antenna, perfect polarization match, and perfect
impedance match at both antennas. At a frequency of 2 GHz, determine the:
(a) power density (in watts/m²) incident on the receiving antenna.
(b) power received by the ground-based antenna whose gain is 60 dB.
Determine VO during the Negative Half Cycle of the input voltage,
Vi
12 V
f = 1 kHz
-12 V
C
...
+
0.1 με
Si
R
56 ΚΩ
Vo
Vi
2 V
-
0
+
Chapter 1 Solutions
Electrical Motor Controls for Integrated Systems
Ch. 1.1 - Prob. 1CPCh. 1.1 - Prob. 2CPCh. 1.1 - Prob. 3CPCh. 1.1 - Prob. 4CPCh. 1.1 - Prob. 5CPCh. 1.1 - Prob. 6CPCh. 1.1 - Prob. 7CPCh. 1.1 - Prob. 8CPCh. 1.1 - Prob. 9CPCh. 1.1 - Prob. 10CP
Ch. 1.1 - Prob. 11CPCh. 1.1 - Prob. 12CPCh. 1.1 - Prob. 13CPCh. 1.1 - Prob. 14CPCh. 1.1 - Prob. 15CPCh. 1.2 - Prob. 1CPCh. 1.2 - Prob. 2CPCh. 1.2 - Prob. 3CPCh. 1.2 - Prob. 4CPCh. 1.2 - Prob. 5CPCh. 1.2 - Prob. 6CPCh. 1.3 - Prob. 1CPCh. 1.3 - Prob. 2CPCh. 1.3 - Prob. 3CPCh. 1.3 - Prob. 4CPCh. 1.3 - Prob. 5CPCh. 1.4 - Prob. 1CPCh. 1.4 - Prob. 2CPCh. 1.4 - Prob. 3CPCh. 1.4 - Prob. 4CPCh. 1.4 - Prob. 5CPCh. 1.4 - Prob. 6CP
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