There's no way for any probe that is sent to orbit/land on a distant body to get there only on precalculated flight parameters alone - minuscule errors in the beginning of flight would convert to huge differences in speed and trajectory near its end. Of course these errors must be corrected during the flight as they become apparent (and before they escalate to uncorrectable levels), but first - they need to become apparent. And while in the initial phase the probes would be able to measure their speed and location quite precisely using the GPS satellites, this is not viable, say, halfway to Saturn, and good few AU away from any near bodies.
So, what methods do the probes use to measure their own flight parameters respective to planned ones?