Attitude determination system with sequencing antenna inputs

• US 5,917,448 A
• Filed: 08/07/1997
• Issued: 06/29/1999
• Est. Priority Date: 08/07/1997
• Status: Expired due to Term

• Current Assignee: Teledyne Scientific & Imaging, LLC (Teledyne Technologies Incorporated)
• Original Assignee: Rockwell Science Center, Inc.
• Inventors: Mickelson, Wilmer A.
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/908,418
• Time in Patent Office: 691 Days
• Field of Search: 342/133, 342/139, 342/140, 342/146, 342/147, 342/434, 342/442, 342/424
• US Class Current: 342/442
• CPC Class Codes: G01S 19/36 relating to the receiver frond end
• CPC Class Codes: G01S 19/53 Determining attitude

Abstract

An attitude determination system uses multiple antenna inputs which are time-multiplexed into a multi-channel receiver. Each channel tracks one incoming signal from a known or ascertainable source. For each of the incoming signals being tracked, digital processing can be used to determine range differences between the different antenna elements for that incoming signal, and to compute attitude based on the range differences and the known configuration of the attenna elements relative to each other.

Claims

1. An attitude determination system for determining attitude of a platform, the system comprising:

a plurality of antenna elements, each of the antenna elements being configured to receive a plurality of incoming signals;

a multiplexer which time-multiplexes among antenna signals received respectively by each of the antenna elements;

a plurality of channels to which a received signal is applied, the received signal coupled from an output of the multiplexer, each of the channels capable of tracking at least one of the incoming signals respectively;

a phase difference processor which determines phase differences between at least some of the antenna elements, for at least one of the incoming signals being tracked; and

an attitude calculator which computes attitude of the platform based on the phase differences.

2. An attitude determination system as set forth in claim 1, further comprising a signal conditioner which converts carrier frequencies of the time-multiplexed antenna signals from transmission frequencies to intermediate frequencies.

3. An attitude determination system as set forth in claim 1, wherein at least one of the channels synchronizes a locally generated code with an incoming code which modulates the incoming signal being tracked in said at least one channel.

4. An attitude determination system as set forth in claim 1, wherein the channels generate control commands in tracking the incoming signals, and the phase difference processor integrates the control commands over a sampling time interval.

5. An attitude determination system as set forth in claim 1, wherein the phase difference processor cancels system biases by subtracting measurements related to phase differences between a single pair of the antenna elements for different incoming signals.

6. An attitude determination system as set forth in claim 1, wherein computing of the attitude of the platform is based further on platform navigation information derived from signals available from the channels.

7. An attitude determination system for determining attitude of a platform, the system comprising:

means for receiving et plurality of incoming signals, said receiving means having a plurality of elements;

means for time-multiplexing among antenna signals received respectively by each of the elements of the receiving means;

means for applying a received signal to a plurality of channels, the received signal coupled from an output of the multiplexing means;

means for tracking at least one of the incoming signals in each of the channels respectively;

means for determining phase differences between at least some of the elements of the receiving means, for at least one of the incoming signals being tracked; and

means for computing attitude of the platform based on the phase differences.

8. An attitude determination system as set forth in claim 7, wherein the tracking means generates control commands in tracking the incoming signals, and the determining means integrates the control commands over a sampling time interval.

9. A method for determining attitude of a platform, the method comprising the steps of:

receiving a plurality of incoming signals by a plurality of antenna elements;

time-multiplexing among antenna signals received respectively by each of the antenna elements;

applying a received signal to a plurality of channels, the received signal coupled from an output produced by the multiplexing step;

tracking at least one of the incoming signals in each of the channels respectively;

determining phase differences between at least some of the antenna elements, for at least one of the incoming signals being tracked; and

computing attitude of the platform based on the phase differences.

10. A method for determining attitude of a platform as set forth in claim 9, further comprising the step of converting carrier frequencies of the time-multiplexed antenna signals from transmission frequencies to intermediate frequencies.

11. A method for determining attitude of a platform as set forth in claim 9, wherein the time-multiplexing step occurs at a rate no greater than approximately 10 Hertz.

12. A method for determining attitude of a platform as set forth in claim 9, wherein the time-multiplexing step occurs at a rate no greater than approximately 1 Hertz.

13. A method for determining attitude of a platform as set forth in claim 9, wherein, in at least one of the channels, the tracking step includes synchronizing a locally generated code with an incoming code which modulates the incoming signal being tracked in said at least one channel.

14. A method for determining attitude of a platform as set forth in claim 9, wherein the tracking step includes generating control commands in tracking the incoming signals, and the determining step includes integrating the control commands over a sampling time interval.

15. A method for determining attitude of a platform as set forth in claim 14, wherein a sampling rate for integrating the control commands is synchronized with a multiplexing rate in the multiplexing step, the multiplexing rate being no greater than the sampling rate.

16. A method for determining attitude of a platform as set forth in claim 9, wherein the determining step is accomplished using digital processing.

17. A method for determining attitude of a platform as set forth in claim 9, wherein the determining step cancels system biases by subtracting measurements related to phase differences between a single pair of the antenna elements for different incoming signals.

18. A method for determining attitude of a platform as set forth in claim 9, wherein the computing step is based further on platform navigation information derived from signals available from the tracking step.

19. A method for determining phase differences for an incoming signal between a plurality of antenna elements, the method comprising the steps of:

time-multiplexing among antenna signals received respectively by each of the antenna elements, each of the antenna signals including the incoming signal;

using a loop phase error signal to track the incoming signal included in a received signal, the received signal coupled from an output produced by the multiplexing step; and

integrating a control command over a sampling time interval, the control command derived from the error signal, a sampling rate in said integrating step being synchronized with a multiplexing rate in the multiplexing step, the multiplexing rate being no greater than the sampling rate.

20. A system for determining phase differences for an incoming signal between a plurality of antenna elements, the system comprising:

a multiplexer which time-multiplexes among antenna signals received respectively by each of the antenna elements, each of the antenna signals including the incoming signal;

a channel which uses a loop phase error signal to track the incoming signal included in a received signal, the received signal coupled from an output of the multiplexer; and

a processor which integrates a control command over a sampling time interval, the control command derived from the error signal, a sampling rate of the processor being synchronized with a multiplexing rate of the multiplexer means, the multiplexing rate being no greater than the sampling rate.