Method of bearing determination utilizing a bottom antenna in an aircraft tracking system

• US 5,235,336 A
• Filed: 09/27/1991
• Issued: 08/10/1993
• Est. Priority Date: 09/27/1991
• Status: Expired due to Term

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Stayton, Gregory T., Sturm, Patricia K.
• Primary Examiner(s): Tubbesing, T. H.
• Application Number:
  US07/767,007
• Time in Patent Office: 683 Days
• Field of Search: 342/30, 342/37
• US Class Current: 342/30
• 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

In a Traffic Alert and Collision Avoidance System on an aircraft having a plurality of antennas, an optimal bearing value is obtained for each target aircraft by generating a target data block for each response to an interrogation, each target data block including a measured bearing value and an associated priority code. A priority code is assigned based on the antenna receiving the information, and the number of valid bearing measurements used to determine a measured bearing value for the reply. If more than one target data block is obtained in a surveillance period, one target data block is retained based on predetermined criteria. The measured bearing value of all the target data blocks having the same, highest priority code are selected or combined, the result being saved in the target data block. The priority codes are then used to select the proper reply bearing measurement, the bearing track update filtering parameters, and to aid in the reply qualification for bearing track initialization.

Claims

1. In an aircraft having a Traffic Alert and Collision Avoidance System (TCAS), said aircraft including a first and second antenna, wherein said aircraft interrogates all target aircraft in the vicinity of said aircraft such that in a surveillance period a predetermined number of interrogations are made during an interrogation portion of the surveillance period, each interrogation being transmitted between said first antenna and said second antenna in a predetermined sequence, said target aircraft responding to each interrogation received such that the same target aircraft responds at least once during a surveillance period, a method for obtaining an optional bearing value for each target aircraft comprising the steps of:

a) generating a target data block for each response received, each target data block including a measured bearing value and an associated priority code;

b) storing the generated target data blocks in a response list;

c) upon completion of the interrogation portion of the surveillance period, determining the target data blocks which relate to the same target;

d) if only one target data block is found in the response list from step (c),

i) retaining that target data block;

otherwise

e) if more than one target data block is found in the response list from step (c),

i) retaining one target data block in the response list based on predetermined criteria;

ii) combining the measured bearing value of all the target data blocks from step (c) having the same, highest priority code thereby obtaining the optimal bearing value; and

iii) storing the resultant optimal bearing value of step (e, ii) in the retained target data block, along with the priority code of the measured bearing value used in step (e, ii); and

f) repeating step (c) until all detectable duplicate target data blocks for each reponding target aircraft have been eliminated from the response list, each remaining target data block having the optimal bearing value and having an associated priority code for tracking each target aircraft.

2. A method for obtaining an optimal bearing value for each target aircraft according to claim 1, wherein the step of generating a target block comprises the steps of:

a) calculating a return bearing value of each of a predetermined number of pulses received from the interrogation,

b) if a first predetermined number of return bearing values are within a predetermined number of degrees (in angular measurements of each other, combining each of the return bearing values to obtain the measured bearing value for storing in the target data block, otherwise, setting the measured bearing value to invalid; and

c) if the interrogation was from the first antenna, tagging the measured bearing value with a first priority code, otherwise, tagging the measured bearing value with a second priority code, the first priority code having a higher priority than the second priority code.

3. A method for obtaining an optimal bearing value for each target aircraft according to claim 2, further comprising the steps of:

a) before the step of calculating, determining if a predetermined non-obstructive condition of the aircraft exists;

b) if so, continuing with the step of calculating;

otherwise, determining if the reply pulses were received from the first antenna; and

c) if so, continuing with the step of calculating, otherwise, marking the measured bearing value as invalid.

4. A method for obtaining an optimal bearing value for each target aircraft according to Claim 3, wherein the step of combining each of the return bearing values comprises the step of:

averaging each of the return bearing values.

5. A method for obtaining an optimal bearing value for each target aircraft according to Claim 1, wherein a plurality of reply pulses are received by the aircraft in response to an interrogation, and further wherein the step of generating a target block comprises the steps of:

a) calculating a return bearing value on each of a first predetermined number of reply pulses, wherein the first predetermined number of reply pulses includes a second predetermined number of expected reply pulses;

b) if the first predetermined number of reply pulses are within a predetermined number of degrees of each other, combining each of the return bearing values to obtain the measured bearing value for storing in the target data block, and proceeding to step (e), otherwise;

c) determining those first predetermined number of return bearing values that are within the predetermined number of degrees of each other,

d) combining those return bearing values determined from step (c) to obtain the measured bearing value, and if none were determined from step (c), marking the measured bearing value invalid; and

e) as a function number of return bearing values utilized to generate the measured bearing value, and the antenna from which the reply pulses were received, assigning a priority code to the measured bearing value stored in the track data bock wherein the highest priority code has the highest degree of confidence in the quality of the measured bearing value.

6. A method for obtaining an optimal bearing value for each target aircraft according to claim 5, further comprising the step of:

a) before the step of calculating, determining if a predetermined non-obstructive condition of the aircraft exists;

b) if so, continuing with the step of calculating;

otherwise, determining if the reply pulses were received from the first antenna; and

c) if so, continuing with the step of calculating, otherwise, marking the measured bearing value as invalid.

7. A method for obtaining an optimal bearing value for each target aircraft according to claim 6, wherein the step of combining each of the return bearing values comprises the step of

averaging each of the return bearing values.

8. A method for obtaining an optimal bearing value for each target aircraft according to claim 1, further comprising the steps of:

a) updating existing tracks wherein the optimal bearing value in the response list is within a predetermined window, said predetermined window being based on said priority code; and

b) initiating new tracks from three successive responses utilizing optimal bearing value information in the response list having at least a predetermined priority code.