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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 />

1<br />

Peak power at 15 and 200 m<br />

Peak power (W)<br />

0.01<br />

1 . 10 3<br />

1 . 10 4<br />

1 . 10 5<br />

1 . 10 6<br />

1 . 10 7<br />

0.1<br />

0 20 40 60 80 100<br />

f (GHz)<br />

range = 15 m<br />

range = 200 m<br />

Figure 4-16: Peak Transmitter Power Required <strong>for</strong> Obstacle Detection at 15 m and 200 m<br />

as a Function of Frequency<br />

Average power at 15 and 200 m<br />

1.10 3 range = 15 m<br />

Average power (W)<br />

1.10 4<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 = 200 m<br />

Figure 4-17: Average Transmitter Power Required <strong>for</strong> Obstacle Detection at 15 m and<br />

200 m as a Function of Frequency<br />

4.3.6.2 Altimetry Results<br />

The altimetry requirements are the most stringent <strong>for</strong> range resolution because altimetry readings<br />

will be used <strong>for</strong> landing. The minimum-range resolution is 6 cm when the Entomopter is<br />

within 3 m of the ground.<br />

The following assumptions were made:<br />

Table 4-2: Parameters <strong>for</strong> Altimetry Analysis<br />

Effective target cross section, σ (m 2 ) 1<br />

Temperature of receiver To (Kelvin) 290<br />

Range resolution, ∆Rmin (m) 0.06<br />

Isotropic gain of transmitting antenna G T (dBi) 8<br />

253

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