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Pseudolite Research

APL Error Modeling

Using APL data requires to be aware of some special features. For example, signal dynamics are much higher than for satellite signals. APL signals have to be acquired in a distance of tens of miles, but also in the vicinity of the airport. This phenomenon is refered to as near-far problem and requires a careful configuration and setting of the whole system. Furthermore, it has to be taken into account that there might be no direct line-of-sight between (the negative elevated) APL and a top-mounted aircraft antenna.

The investigated potential errors are:

  • tropospheric error

  • signal creeping error

  • bias error

The tropospheric component is due to the diverging signal paths of APL and satellite signals, the signal creeping component is due to signal reception without line-of-sight induced by the conducting surface of the fuselage, and the reference receiver bias component is due to remaining problems with the near-far problem. The error model provides corrections for APL code and phase measurements.

fusel

Analytical determination of the signal creeping effect on the pseudorange regarding a Dornier Do 128 aircraft in relation to the roll angle PHI and the geometrical angle ALPHA which is the azimuth difference between the longitudinal axis of the aircraft and the direction to the APL.







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