Aircraft collision avoidance system

• US 4,710,774 A
• Filed: 02/18/1986
• Issued: 12/01/1987
• Est. Priority Date: 02/18/1986
• Status: Expired due to Fees

• Current Assignee: Gunny Family Trust Dated August 1 1991
• Original Assignee: Edmond R. Gunny
• Inventors: Gunny, Edmond R.
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Cain, David
• Application Number:
  US06/830,629
• Time in Patent Office: 651 Days
• Field of Search: 342/455, 342/88, 342/29, 342/454, 364/460, 364/461
• US Class Current: 342/455
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft

Abstract

A communication system particularly adapted for use in an aircraft collision avoidance system wherein the transmitted portions of messages exchanged between aircraft consist of pulses or pairs of pulses at the beginning and end of a message. The data or information content of a message is defined by the time duration between start and end pulses, an interval during which the sender'"'"'s transmitter is off. Thus the media is clear for other aircraft to use during the major portion of any message, thereby greatly increasing the number of aircraft which can be accommodated by the system without overloading the communication medium. The system provides for determining the presence of other aircraft in the near vicinity which may be a collision threat and for sending intent messages to threat aircraft to assist in collision avoidance.

Claims

1. An aircraft collision avoidance system in which a plurality of aircraft are equipped with radio communication systems, each such communication system comprising:

message receiving and transmitting means;

data processing means coupled to the transmitting means for generating plural-data-content interrogation messages in accordance with a first selected format and for generating reply messages in accordance with a second selected format;

said data processing means further including means for decoding a received interrogation message according to said first format and means for initiating generation of a reply message thereto in said second format if and only if the data decoded from said received interrogation message indicates proximity of the interrogating aircraft to the receiving aircraft within preselected limits;

wherein said first and second formats comprise brief initiation and termination pulses spaced apart by a time duration of silence corresponding to the data content of the message.

2. The system of claim 1 wherein the position of the termination pulse is variable, relative to the position of the initiation pulse, in accordance with the data to be conveyed in the message.

3. The system of claim 1 wherein the interrogation message includes a first pair of pulses to initiate the message and a second pair of pulses to terminate the message to distinguish the interrogation message from a reply message which contains only a single initiation pulse and a single termination pulse.

4. The system of claim 3 wherein the second pair of pulses terminating the interrogation message is spaced differently from the first pair of pulses initiating the interrogation message in order to provide a unique identification for the respective initiation and termination pulses.

5. The system of claim 4 wherein a reply message may have tacked onto it an optional intent message which terminates with a pair of pulses which are spaced differently from either pair of pulses in an interrogation message, the time duration of the optional part between the termination pulse of the reply message and the first pulse of said termination pair of the intent message being equal to some multiple of a reference time interval according to an intended evasive maneuver of the replying aircraft in a threat situation.

6. The system of claim 1 wherein the data processing means includes means for generating a sysem clock signal and wherein each of the first and second message formats includes a plurality of portions corresponding respectively to different types of data within a message, the duration of a first one of said portions being measured in multiples of unit times up to a predetermined maximum number defining the block, where a unit time is equal to the period of said clock signal, and the duration of a second one of said portions being measured in multiples of said blocks up to a predetermined maximum.

7. The system of claim 6 wherein the second message format further includes a third portion which is measured in multiples of a sub-block, said sub-block having a duration equal to some multiple of unit times which is less than the number of unit times in a block.

8. The system of claim 7 further including means for counting the number of unit times in a received message in binary numbers and means for storing the resulting count in a binary register such that the count of a first portion of the register is available as a direct indication of one type of received data and the count of another portion of the register is available as a direct indication of another type of received data.

9. The system of claim 1 wherein each of the first and second message formats includes a first portion equal to a number of unit times corresponding to the value of a first type of data to be transmitted, said number of unit times being within a range assigned for the transmission of the first type of data, and a second portion equal to a number of blocks of unit times which corresponds to the value of a second type of data to be transmitted, each of said blocks being equal to the number of unit times defining the upper limit of said first type of data.

10. The system of claim 9 wherein the interrogation message includes data indicating the altitude to be attained by the interrogating aircraft some predetermined time period following transmission of the interrogation message and data indicating the type of interrogating aircraft.

11. The system of claim 10 wherein the altitude data is represented by a time duration equal to a number of unit times which is between zero and a predetermined upper limit and wherein the time duration indicating the type of aircraft is equal to a number of blocks within a range from zero to a predetermined upper limit according to type, a block being equal in time duration to the upper limit of unit times in said altitude range.

12. The system of claim 11 wherein the altitude data is represented by a time duration in the range from 0 to 511 unit times and wherein the type of aircraft is represented by a time duration equal to a number of 512-unit-time blocks in the range from 0 to 3.

13. The system of claim 9 wherein future differential altitude is represented by a time duration equal to a number of unit times between 0 and 127, wherein aircraft type is represented by a time duration equal to a number of 128-unit-time blocks between 0 and 3, and wherein the address of the interrogating aircraft to which the reply message is directed is represented by a time duration equal to a number of 512-unit-time blocks between 0 and 15.

14. The system of claim 13 wherein the address data contained in a reply message corresponds to the least four significant digits in the altitude data portion of the interrogation message which is being replied to.

15. The system of claim 5 having a time reference clock and wherein the data processing means further includes means for generating a signature to identify the pulses of a received message upon detection of an initiation pulse of said message comprising means for storing levels of selected parameters of the detected pulse and means for comparing the levels of the same selected parameters of a subsequently received pulse with the stored levels of a previously received pulse to determine if the pulses are part of the same message.

16. The system of claim 15 wherein one of the selected parameters of a detected pulse is signal strength.

17. The system of claim 16 wherein another selected parameter of a detected pulse is phase of the pulse relative to a timing reference signal.

18. The system of claim 17 further including a phase reference clock operating at some integral multiple of the time reference clock rate and means for storing a count of phase reference clock pulses relative to the period of the time reference clock upon detection of a signal which is part of a received message.

19. A data processor for periodically generating interrogation messages for transmission over a common medium which is shared by messages from other sources and for generating reply messages to received interrogation messages, the data processor comprising:

means for generating interrogation messages having a first start pulse configuration and a first termination pulse configuration which are capable of identifying interrogation messages, the time duration between the first start and termination pulse configurations establishing the information content of the message;

means for generating a replay message having a second start pulse configuration and a second termination pulse configuration in reply to a received interrogation message, said second configurations being capable of identifying reply messages, the time duration between the second start and termination pulse configurations establishing the information content of the reply message;

means for determining the type of received message;

means for decoding the respective types of received message to determine the information content thereof; and

means for initiating the generation of a reply message upon the decoding of a received interrogation message.

20. The data processor of claim 19 wherein the message generating means include means for modulating the time duration of the message in accordance with the magnitudes of a plurality of selected parameters which are to be conveyed in the message such that the message information is conveyed by the time duration of a period of non-transmission between beginning and ending pulses of the message.

21. The data processor of claim 20 further including means for sending messages overlapping in time by transmitting a start pulse of one message in the time interval between the start and termination pulses of another message.

22. The data processor of claim 21 wherein the interrogation message decoding means include means for distinguishing the start pulse pair and the termination pulse pair of a received interrogation message.

23. The data processor of claim 22 wherein the interrogation message decoding means include means for separately storing the start pulse pairs of received interrogation messages and means for matching the termination pulse pairs with the corresponding start pulse pairs of respective received interrogation messages so that a plurality of overlapping received interrogation messages may be decoded.

24. The data processor of claim 23 wherein the interrogation message decoding means further include means for concurrently decoding the message content of a plurality of interrogation messages which are received concurrently with overlapping time intervals.

25. The data processor of claim 19 for use in an aircraft collision avoidance system wherein altitude information is conveyed as part of the content of transmitted messages, the altitude information of an interrogation message being the altitude to be attained by the interrogating aircraft at a preselected future time.

26. The data processor of claim 25 wherein the altitude information conveyed in a reply message represents the difference between the altitude which will be attained by the responding aircraft at a preselected future time and the future attained altitude of the interrogation message being replied to.

27. The data processor of claim 26 wherein interrogation messages include data corresponding to future altitude and aircraft type of the interrogating aircraft, the two types of data being represented by time intervals which are added together to form the interrogation message represented between the start and termination pulse pairs of the message.

28. The data processor of claim 27 wherein an interrogation message from a ground station is designated by a predetermined one of the available aircraft type assignments in the aircraft type portion of the message.

29. The data processor of claim 28 wherein the reply message generator is only responsive to interrogation messages from aircraft within a predetermined altitude range of the responding aircraft.

39. The data processor of claim 19 wherein the first start and termination pulse configurations each comprise a pair of pulses, and wherein the second start and termination pulse configurations each comprise a single pulse.

30. The method of generating a message for transmission via a shared medium comprising:

generating a start pulse to indicate the beginning of the message;

generating a termination pulse to indicate the end of the message; and

controlling the spacing between the start pulse and the termination pulse in accordance with the information content of the message.

31. The method of claim 30 wherein the message comprises a plurality of different types of data, the data within a given type being variable within a predetermined range.

32. The method of claim 31 wherein the data of one type is represented by a number of unit times duration within a first range, and wherein the data of another type is represented by a number of unit time blocks duration within a second range, each block being a multiple of unit times equal to the upper limit of the number of unit times in the first range.

33. The method of claim 32 wherein a portion of the message is represented by numbers of unit time blocks within a third range, each such block being a number of unit times which is a sub-multiple of the unit times in the blocks of the second range.

34. The method of claim 30 further including the steps of generating messages of different types and distinguishing the different types of messages by varying the numbers of start and termination pulses.

35. The method of claim 34 including generating an interrogation message by placing a pair of start pulses at the beginning of the message, which pulses are separated by a first interval, and placing a pair of termination pulses at the end of the message, the termination pulses being separated by a second interval which is a selected multiple of the first interval.

36. The method of claim 35 wherein the message is a reply to an interrogation message and is followed by an intent message which is terminated by a pair of pulses separated by a third interval, the third interval being a selected multiple of the first interval which is different from the second interval to assure discrimination between the types of messages.

37. The method of processing messages generated in accordance with the method of claim 30 comprising:

identifying a received pulse as the start of a message;

beginning a count of unit times upon receipt of said start pulse;

developing a pulse signature from said start pulse on the basis of a plurality of selected parameters;

comparing other received pulses with the signature of said start pulse;

terminating said unit time count upon recognition of a termination pulse having a signature corresponding to that of the start pulse; and

decoding the received message from the time interval between the start and termination pulses.

38. The method of claim 37 further including the steps of identifying the received message as an interrogation message upon receipt of a start pulse pair and identifying the termination of the message upon detection of a termination pulse pair having a signature corresponding to that of the start pulse pair.