Collision avoidance system of aircraft

• US 4,167,006 A
• Filed: 10/19/1977
• Issued: 09/04/1979
• Est. Priority Date: 10/22/1976
• Status: Expired due to Term

• Current Assignee: TOYO Tsushinki Kabushiki Kaisha
• Original Assignee: TOYO Tsushinki Kabushiki Kaisha
• Inventors: Hirata, Toshikiyo, Funatsu, Chuhei
• Primary Examiner(s): Tubbesing, T. H.
• Application Number:
  US05/843,657
• Time in Patent Office: 685 Days
• Field of Search: 343/6.5 LC, 343/112 CA
• US Class Current: 342/32
• CPC Class Codes: G01S 13/781 Secondary Surveillance Radar [SSR] in general

Abstract

A collision avoidance system for aircraft using an on-board beacon interrogator. If altitude information is not included in a response signal from a transponder of an other aircraft or the response signal is garbled because a plurality of other aircraft are responding to the same interrogation signal, the system automatically switches to a beacon based proximity warning system and indicates the distance or other indication to the detected aircraft.

Claims

1. In a collision avoidance system for aircraft equipped with transponders which transmit response signals to interrogations from interrogating aircraft, means within the interrogating aircraft operative on receipt from an interrogated aircraft of response signals which contain information denoting a threat condition for indicating to the interrogating aircraft pilot, as a beacon based collision avoidance indication, a direction to navigate to avoid collision, and means within the interrogating aircraft operative on receipt from the interrogated aircraft or response signals from which desired elevation information is absent for automatically switching from said beacon based collision avoidance indication to a beacon based proximity warning indication for indicating one or more of (a) the distance between the interrogating and the interrogated aircraft, (b) the approaching speed of the aircraft, (c) time to collision or (d) relative flying direction.

2. In the system of claim 1, wherein three delay lines are provided each having a predetermined time delay corresponding to the time interval between framing pulses of the response signal from the transponder of interrogated aircraft, each delay line having intermediate taps of predetermined time interval, the delay lines being connected in a series circuit.

3. In the system of claim 2, wherein the center of the three series connected delay lines has an input and an output which are supplied to an AND gate whose output signal represents receipt of a response signal, said intermediate taps of said center delay line being connected to an OR gate, the non-existence of an output signal from said OR gate with an output from said AND gate denoting the absence of altitude information whereby to cause said second-named means to switch from the beacon based collision avoidance indication to the beacon based proximity warning indication.

6. In the system of claim 3, wherein the center of the three series connected delay lines has an input and an output which are supplied to an AND gate whose output signal represents receipt of a response signal, and wherein a delay line preceding or succeeding the center delay line has a signal output from their intermediate taps, said signal output representing a superposition of response signals from interrogated aircraft and effects operation of said second-named means to switch from the beacon based collision avoidance indication to the beacon based proximity warning indication.

4. In a collision avoidance system for aircraft equipped with transponders which transmit response signals to interrogations from interrogating aircraft, means within the interrogating aircraft operative on receipt from an interrogated aircraft of said response signals for indicating to the interrogating aircraft pilot, as a beacon based collision avoidance indication, a direction to navigate to avoid collision, and means within the interrogating aircraft operative on receipt from a plurality of transponders in interrogated aircraft of response signals having framing pulses, within which the respective response signals are superposed, for automatically switching from said beacon based collision avoidance indication to a beacon based proximity warning indication for indicating one or more of (a) the distance between the interrogating and the interrogated aircraft, (b) the approaching speed of the aircraft, (c) time to collision or (d) relative flying direction.

5. In the system of claim 4, wherein three delay lines are provided each having a predetermined time delay corresponding to the time interval of said framing pulses, each delay line having intermediate taps of predetermined time interval, the delay lines being connected in a series circuit.