Method for realizing, simultaneous reference pulse receiver for wire steered aircraft (drone) with steering wire interface, consisting of reference-pulse-receiver and command transmitter, with special signal-measuring-bridge

摘要

In steering wire is incorporated special signal measuring bridge so set-up that command pulses at bridge output do not deliver any evaluatable measuring signal, while reference pulses, even at simultaneous operation, generate measuring signal at bridge output. Measuring signal is evaluated in pulse discriminator circuit, while locking logic, behind pulse discriminator prevents generation of pseudo reference pulses, which otherwise are formed in relation to so called command discharge pulses. Independent claims are included for simultaneous reference pulse receiver.