Method and system for determining a position of a target vehicle utilizing two-way ranging

• US 5,969,674 A
• Filed: 02/21/1997
• Issued: 10/19/1999
• Est. Priority Date: 02/21/1997
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Inventors: Chang, Donald C. D., von der Embse, Urban A., Huang, Kenneth Yu
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/803,936
• Time in Patent Office: 970 Days
• Field of Search: 342/353, 342/357, 342/458, 342/453, 342/461, 455/441
• US Class Current: 342/357.2
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 13/74 Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems
• CPC Class Codes: G01S 13/878 Combination of several spaced transmitters or receivers of known location for determining the position of a transponder or a reflector G01S13/874 takes precedence
• CPC Class Codes: G01S 19/03 Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
• CPC Class Codes: G01S 19/09 providing processing capability normally carried out by the receiver
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/36 relating to the receiver frond end
• CPC Class Codes: G01S 19/52 Determining velocity
• CPC Class Codes: G01S 5/14 Determining absolute distances from a plurality of spaced points of known location

Abstract

A communication system transmitting messages includes two-way ranging by communicating between a target vehicle and a traffic controller station through a plurality of satellites. A set of the plurality of satellites may be used simultaneously or sequentially to transmit and receive signals from the ground station to a target vehicle, preferably an aircraft in the preferred embodiment. Each aircraft includes a particular ranging code combined with a message signal to selectively process the ranging data supplied to each vehicle. The ranging determination may be used in conjunction with alternative ranging devices, such as a global positioning system, in order to improve the accuracy of the estimations provided by the ranging processing. Nevertheless, the method and apparatus of the present invention provide relatively accurate state vectors without the need for precisely accurate timing synchronization at each of the stations connected by communication links.

Claims

1. A communication system for monitoring the position and velocity of an aircraft, the system comprising:

a control station positioned on earth, the control station having a known position;

at least three satellites orbiting earth and positioned in multiple planes, each of the at least three satellites having a communication link system communicating through a respective first signal link with the control station, wherein a position of each of the at least three satellites is known such that a range between each of the at least three satellites and the control station is known; and

an aircraft having a communications transceiver for sending and receiving signals to and from each of the at least three satellites through a second signal link corresponding to a respective first link, each of the corresponding first and second signal links defining a path for carrying a signal between the aircraft and the control station via a respective one of the at least three satellites, wherein each of the paths is a two-way communication between a respective one of the at least three satellites and each of the control station and the aircraft, wherein each signal includes a unique Auslander-Barbano code division multiple access (AB CDMA) signal portion assigned to the aircraft and a data message portion, the data message portion being modulated by a wavelet-based finite-impulse-response (WFIR) waveform with the AB CDMA signal portion;

wherein the control station includes a dual alpha-beta/extended Kalman-filter tracking loop which processes the signals to determine a range between each of the at least three satellites and the aircraft as a function of time for the signals to travel the paths, the position of the aircraft as a function of the ranges and the known positions of the control station and the at least three satellites, and the velocity of the aircraft as a function of Doppler shift of each of the signals during travel of the paths.

4. The system of claim 1 wherein:

the alpha-beta tracking loop includes time and frequency tracking loops.

2. The system of claim 2 wherein:

the aircraft further includes a retrodirective antenna for transmitting and receiving signals to and from the at least three satellites, wherein the retrodirective antenna determines direction of a signal received from one of the at least three satellites and transmits a signal to the one of the at least three satellites back along the direction of the received signal.

3. The system of claim 2 wherein:

the retrodirective antenna includes a Butler matrix, a digital beam former, and a wavelet-based finite-impulse-response (WFIR) signal processor.