POWER CONTROL OF PSEUDOLITES WHILE LANDING AN AIRCRAFT
Abstract
The effect of a pseudolite (PL) signal on quality of functioning of the GLONASS/GPS receivers of satellite navigation has been researched and experimental confirmation of near-far effect developing with the help of NI GPS Simulation Toolkit hardware and software has been obtained. An algorithm of an optimal power control has been obtained. PL based on the evaluation of the signal delay time in data transfer line has been synthesized. The analysis of the simulation results showed that the implementation of the proposed optimal control algorithm allows eliminating the effect “near-far” developing and ensuring simultaneous reception of signals of GLONASS/GPS satellite and PL.
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Review
For citations:
Erokhin V.V. POWER CONTROL OF PSEUDOLITES WHILE LANDING AN AIRCRAFT. Civil Aviation High Technologies. 2016;(226):54-61. (In Russ.)
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