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Phase II Final Report - NASA's Institute for Advanced Concepts

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Chapter 4.0 Entomopter Flight Operations<br />

4.3 Entomopter-borne Active Emitters <strong>for</strong> Navigation and Communication<br />

Average power at 200 and 1000 m<br />

1.10 4 range = 200 m<br />

Average power (W)<br />

1.10 5<br />

1.10 6<br />

1.10 7<br />

1.10 8<br />

1.10 9<br />

1.10 10<br />

1.10 11<br />

1.10 12<br />

0 20 40 60 80 100<br />

f (GHz)<br />

range = 1000 m<br />

Figure 4-23: Average Transmitter Power Required <strong>for</strong> Communications at 200 and<br />

1,000 m as a function of Frequency<br />

The peak power will remain constant with bit rate and interpulse period. However, the average<br />

power will vary. The required average powers <strong>for</strong> 200-m and 1,000-m ranges are plotted versus<br />

data rate at 18 GHz in Figure 4-24. The range of data rates in Figure 4-24 corresponds to interpulse<br />

periods T of 10,000 T w (dt = 1/10,000) to 100 T w (dt = 1/100).<br />

0.01<br />

Average power at 200 and 1000 m<br />

Average power (W)<br />

1 . 10 3<br />

1 . 10 4<br />

1 . 10 5<br />

1 . 10 6<br />

0 0.5 1 1.5 2 2.5 3<br />

data rate (Mbits/second)<br />

range = 200 m<br />

range = 1000 m<br />

Figure 4-24: Average Transmitter Power Required <strong>for</strong> Communications at 200-m and<br />

1,000-m as a Function of Data Rate<br />

Power consumption <strong>for</strong> positioning will not take place on board the Entomopter. It will be per<strong>for</strong>med<br />

from the rover.<br />

4.3.7 Future Development Path <strong>for</strong> the Active Communications<br />

Option<br />

In the area of the communications/control subsystem option, future development would include<br />

the design and development of the subsystem components including the transmitter, receiver,<br />

and antennas. The proposed subsystem uses extremely short, wideband, rapid sequences of RF<br />

257

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