System of an aircraft collision avoidance system for suppressing useless alarms

• US 5,202,684 A
• Filed: 04/19/1990
• Issued: 04/13/1993
• Est. Priority Date: 10/17/1985
• Status: Expired due to Fees

• Current Assignee: Miyazaki Epson Corp.
• Original Assignee: Miyazaki Epson Corp.
• Inventors: Funatsu, Chuhei
• Primary Examiner(s): Ng, Jin F.
• Assistant Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US07/511,321
• Time in Patent Office: 1,090 Days
• Field of Search: 340/961, 340/963, 364/461, 342/29, 342/30, 342/32, 342/33, 342/455
• US Class Current: 340/961
• CPC Class Codes: G01S 13/782 using multimoding or selective addressing
• CPC Class Codes: G01S 13/91 for traffic control G01S13/93 takes precedence
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00

Abstract

The present invention is concerned with a system in which when the altitude of a subject aircraft becomes lower than a predetermined altitude, a warning limit value is reduced or made equal to zero on the minimum altitude side whereby a useless alarm based on response signals delivered from other aircraft staying in or taxiing in the airport are suppressed.

Claims

1. A system for suppressing useless alarms of an aircraft collision avoidance system which has a function of determining whether or not a subject aircraft is in danger of colliding with another aircraft and which generates an alarm when it has determined that the subject aircraft is in danger of colliding with another aircraft, through utilization of a response signal received from the other aircraft, said system for suppressing useless alarms comprising a variable threshold generator and said collision avoidance system comprising:

a receiver for receiving at least said response signal from the other aircraft;

a collision avoidance system logic circuit which receives said response signal received by said receiver and which is controlled in accordance with a threshold valve output by said variable threshold generator, said logic circuit for actuating an alarm when a difference between an altitude of the other aircraft denoted by said response signal and an altitude of said subject aircraft is within the threshold value; and

a display which is controlled by an output of said collision avoidance system logic circuit;

said system for suppressing useless alarms comprising;

an altitude information detector for obtaining altitude information of said subject aircraft;

an encoder for encoding an output of said altitude information detector into a coded signal; and

,

said variable threshold generator is controlled in response to said coded signal output by said encoder of said altitude information detected by said altitude information detector;

wherein when said subject aircraft descends to a predetermined altitude, the threshold value output by said variable threshold generator is reduced according to an altitude of said subject aircraft so as to thereby prevent an alarm from being generated on the basis of said response signal from said other aircraft located at an altitude which is lower than an altitude value resulting from subtracting said threshold value from said altitude of said subject aircraft, whereby the generation of a useless alarm is suppressed.

2. A system for suppressing useless alarms of an aircraft collision avoidance system which has a function of determining whether or not a subject aircraft is in danger of colliding with another aircraft and which generates an alarm when it has determined that the subject aircraft is in danger of colliding with another aircraft, through utilization of a response signal received from the other aircraft, said system for suppressing useless alarms comprising a variable threshold generator and said collision avoidance system comprising:

a receiver for receiving at least said response signal from the other aircraft;

a collision avoidance system logic circuit which receives said response signal received by said receiver and which is controlled in accordance with a threshold value output by said variable threshold generator, said logic circuit for actuating an alarm when a difference between an altitude of the other aircraft denoted by said response signal and an altitude of said subject aircraft is within the threshold value; and

a display which is controlled by an output of said collision avoidance system logic circuit;

said system suppressing useless alarms comprising;

an altitude information detector for obtaining altitude information of said subject aircraft;

an encoder for encoding an output of said altitude information detector into a coded signal; and

,

said variable threshold generator which is controlled in response to said coded signal output by said encoder of said altitude information detected by said altitude information detector;

wherein when said subject aircraft descends to a predetermined altitude, the threshold value of said variable threshold generator is made equal to zero so as to thereby prevent an alarm from being generated on the basis of said response signal from said other aircraft located at an altitude which is lower than said subject aircraft, whereby the generation of a useless alarm is suppressed.