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The passive air-band receiver is a type of crystal radio which contains no local oscillator which might interferes with the on-board aircraft s sensitive electronics The passive aircraft receiver broadly tunes from 118 MHz to 136 MHz, and was designed to listenin to in-flight communications between your pilot and

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In the bottom equation, we can add the quantity (2 + j3) to each side, getting x = 2 + j3 The roots can be formally expressed this way: x = 2 j3 The solution set is X = {( 2 j3), (2 + j3)} 8 To get the polynomial form of the quadratic stated in Prob 7, we can multiply out the trinomial factors Here s the original equation again: (x + 2 + j3)(x 2 j3) = 0 Let s convert the subtractions in the second factor to negative additions individually to minimize the risk of getting the signs mixed up when we expand the equation into polynomial form That gives us (x + 2 + j3)[x + ( 2) + ( j3)] = 0 Now we can multiply out, obtaining x 2 + ( 2x) + ( j3x) + 2x + ( 4) + ( j6) + j3x + ( j6) + 9 =0 which simplifies to x 2 + ( j12) + 5 = 0 and further to x 2 + (5 j12) = 0 9 Here s the polynomial equation we derived It s interesting, because the coefficient of x is equal to 0, while the stand-alone constant is complex x 2 + (5 j12) = 0 Here are the roots we found: x = 2 j3 or x = 2 + j3 or x = 2 + j3

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Figure 81: L1 C/A position estimate results Left- Plot of the point position estimation error versus time The top curve is north error The middle curve is east error The bottom curve is down error Right- Scatter plot of the north and east estimation error from the estimated position so that the plots illustrate the estimation error The same set of satellites (ie, PRNS: 2, 4, 9, 12, 17, and 28) was used for the duration of the experiment This gure illustrates the character of the positioning accuracy achievable by SPS GPS First, note that the estimate of d is signi cantly noisier than the estimates of n and e Also notice that the position estimation error has signi cant time correlation This is due to the fact that various of the error sources (SV clock and ephemeris error, ionospheric error, and tropospheric error) are slowly time varying This fact is used advantageously in di erential GPS systems as discussed in Section 88 The sources and magni cation of these errors are discussed in the Sections 84 and 85 Third, due to the fact that the error sources are time-correlated over the period of the experiment shown in Figure 81, the scatter plot does not have the characteristics ellipsoidal shape discussed in Section 4912

The passive air-band receiver can be constructed on a regular circuit board or it could be built on a

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x = ( ) (815)

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