Altitude coding for collision avoidance system

Claim 2

An encoder for use at an interrogator station to provide an altitude address for transmission to a remote aircraft for reply thereto by the aircraft if the altitude of the remote aircraft corresponds to the address, comprising in combination; a. means for generating a pair of pulses having spacing between each pulse of said pair of pulses corresponding to a particular altitude address, b. means for periodically changing the spacing between said pair of pulses in accordance with a predetermined program to provide a scan of altitudes of predetermined bands, said pulse pair generating means including means for providing said spacing between said pulses in accordance with discrete changes in altitude of said interrogator station that occur during periods of transmission of said pulses, said discrete changes having a value greater than a predetermined value whereby said pulse pair spacing changes in discrete increments only with altitude changes exceeding said predetermined value.

Claim 3

An encoder according to claim 1 including a digital read-out altimeter and means for computing the rate of change of altitude in response to the digital data output of said altimeter.

Claim 4

An encoder according to claim 2 including a memory device and a modulo-m counter wherein said program is provided by said memory device, the address of said memory device being determined by data corresponding to the output of said digital altimeter and said modulo-m counter.

Claim 5

An encoder according to claim 3 further including a variable output digital delay device wherein said memory device provides output control signals to vary the delay of said device in accordance with the program of said memory, said pulse pair generating means including said delay device arranged to receive and delay a probe signal an interval according to said program, said pulse pair generating means including means to transmit said probe signal as said first pulse of said pair of pulses and subsequently transmit said delayed probe signal as said second signal of said pair of pulses manifesting thereby said altitude address.

Claim 6

A collision avoidance system for use with interrogator and responder aircraft wherein an altitude discriminant is provided in accordance with a predetermined altitude scan schedule comprising in combination: means on an interrogator aircraft for transmitting in accordance with a predetermined schedule of addressed altitudes a pair of probe pulses spaced in accordance with a fixed interval and a variable interval depending upon the barometric altitude of the interrogating aircraft, said pulse pair transmitting means including means for providing said spacing between said pulses in accordance with discrete changes in altitude of said interrogator aircraft that occur during periods of transmission of said pulses, said discrete altitude changes having a value greater than a predetermined value whereby said pulse pair spacing changes in discrete increments only with altitude changes exceeding said predetermined value, means on responder aircraft for receiving said pair of probe pulses, said receiving means including means for delaying said first received pulse of said pair of probe pulses an interval proportionate to the barometric altitude of the replying aircraft, and further means on said responding aircraft for transmitting a reply signal only if the second received pulse of said pair of probe pulses is received at a time substantially corresponding to the end of said delay of said first received pulse.

Claim 7

A collision avoidance system for use with interrogator and responder aircraft wherein an altitude discriminant is provided in accordance with a predetermined altitude scan schedule comprising in combination: means on an interrogator aircraft for transmitting in accordance with a predetermined schedule of addressed altitudes a pair of probe pulses spaced in accordance with a fixed interval and a variable interval depending upon the barometric altitude of the interrogating aircraft, said pulse pair transmitting means including means for providing said spacing between said pulses in accordance with discrete changes in altitude of said interrogator aircraft that occur during periods of transmission of said pulses, said discrete altitude changes having a value greater than a predetermined value whereby said pulse pair spacing changes in discrete increments only with altitude changes exceeding said predetermined value, means on responder aircraft for receiving said pair of probe pulses, said receiving means including means for delaying said first received pulse of said pair of probe pulses an interval proportionate to the barometric altitude of the replying aircraft, and further means on said responding aircraft for transmitting a reply signal only if the second received pulse of said pair of probe pulses is received at a time substantially corresponding to the end of said delay of said first received pulse.

Claim 8

A system according to claim 5 including a digital read-out altimeter on said interrogator aircraft and means for computing a rate of change of altitude of said interrogator aircraft in response to the digital data output of said altimeter.

Claim 9

An encoder according to claim 6 including on said interrogator aircraft a memory device and modulo-m counter wherein said program is provided by said memory device responsive to an input control address, the input control address of said memory device being determined by control signals corresponding to the output of said digital altimeter and said modulo-5 counter.

Claim 10

An encoder according to claim 7 wherein said pair of pulses are spaced in accordance with the output of a variable delay line on said interrogator aircraft, said delay line being responsive to signals representing a memory storing a predetermined program of fixed discrete steps of intervals, each interval representing said predetermined increments of altitude for encoding said address.