Ship heading and pitch using satellite ephemerides and radar range measurement of satellite

• US 8,963,764 B1
• Filed: 01/14/2011
• Issued: 02/24/2015
• Est. Priority Date: 01/14/2011
• Status: Active Grant

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Boardman, Jonathan A., Gray, Jack
• Primary Examiner(s): Sotomayor, John B
• Assistant Examiner(s): WINDRICH, MARCUS E
• Application Number:
  US13/007,244
• Time in Patent Office: 1,502 Days
• Field of Search: 342/41, 342/126, 342/133, 342/357.25, 342/357.26
• US Class Current: 342/41
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 13/874 Combination of several systems for attitude determination in general G01C, control of attitude G05D1/49
• CPC Class Codes: G01S 13/956 mounted on ship or other platform
• CPC Class Codes: G01S 5/0247 Determining attitude

Abstract

There may be situations in which a ship at sea is lost and GPS is not available due to jamming, and neither a position fix nor GPS is available, or the heading and attitude sensors are degraded. A system and method allow estimating a ship'"'"'s heading and pitch using radar range measurements, multiple antennas and satellite ephemeris data.

Claims

1. A method for determining at least one of heading and pitch of a movable platform, said method comprising the steps of:

operating a radar system in communication with a computer, and having receivers mounted at forward and aft positions on said moveable platform, and having a transmitter mounted on at least one of said forward and aft positions on said movable platform, where said forward and aft positions define a baseline, to measure the ranges of at least two satellites, operating said radar system comprising;

transmitting a radar signal from an active radar and receiving said first radar signal at said active radar when said radar signal is reflected off of one of said at least two satellites, said active radar mounted at said forward location; and

receiving by a passive radar receiver said radar signal transmitted by said active radar, wherein said passive radar receiver is mounted at said aft location;

obtaining from a memory coupled to said computer, pre-stored ephemerides for said satellites; and

using said computer and said satellite ephemerides, setting up delta-range equations in said computer expressing a baseline vector in terms of range measurements from said forward and aft positions and said at least two satellites, and determining a least squares solution for the at least one of heading and pitch using the delta-range equations and the range measurements from said forward and aft locations,

wherein said solution for at least one of heading and pitch is determined independently of any off-platform sensors or transmissions.

3. The method of claim 1, wherein a line of sight direction between said forward position and first measured satellite is assumed to be the same line of sight direction between said aft position and said first measured satellite.

4. The method of claim 1, further comprising:

solving for said baseline vector in the computer by performing the steps of;

solving for the baseline vector in the moveable platform'"'"'s navigation reference frame;

comparing said baseline vector in the moveable platform'"'"'s navigation reference frame to the baseline'"'"'s position in the platform'"'"'s body frame;

determining the moveable platform'"'"'s heading in said navigation reference frame based on said comparison.

5. The method of claim 4, wherein said navigation reference frame is a East-North-Up (ENU) reference frame.

6. The method of claim 1, wherein said solution for at least one of heading and pitch is further determined independently of Earth'"'"'s magnetic field.

7. The method of claim 1, further comprising:

in said computer, applying a weight matrix containing a covariance of said delta-range equations based on an uncertainty of the delta-range measurement for each of the at least two satellites to said delta range equations to favor more accurate range measurements over less accurate range measurements.

8. The method of claim 1, wherein the determination of the pitch of the moveable platform is performed when said receivers of said radar platform mounted at said forward and aft positions, are located on a roll axis of said moveable platform.

9. The method of claim 1, wherein a delta range is defined as a difference in range between a first satellite and said first radar receiver mounted at said forward position, and between said first satellite and said second radar receiver mounted at said aft position.

2. A method for determining heading and pitch of a movable platform carrying a first radar arrangement including an antenna located at one of a forward-located and an aft-located position and also carrying a second radar arrangement including an antenna located at the other one of said forward-located and aft-located positions, said method comprising the steps of;

transmitting a radar signal from said first radar arrangement at an active radar mounted at a first of said forward-located and said aft-located positions and receiving said radar signal transmitted from said active radar at said first position;

receiving said radar signal transmitted from said active radar at said second radar arrangement at a passive radar mounted at the other one of said forward-located and aft-located positions;

measuring by said first and second radar arrangements, the range to at least two Earth satellites from said first and second radar arrangements, to form measured ranges;

obtaining from a memory in communication with said computer, ephemeris data for said satellites pre-stored in said memory;

obtaining from a second memory in communication with said computer, an initial estimate of heading and pitch pre-stored in said second memory;

in a computer process, calculating an estimated vector representing a baseline extending between said forward- and aft-located positions independently of any off-platform sensors or transmissions;

in said computer process, calculating estimated range differences between said satellites and said forward and aft locations;

in said computer process, forming a geometry matrix from said ship-satellite geometry;

in said computer process, forming a Jacobian matrix representing variation in the baseline vector;

in said computer process, forming an incremental solution for heading and pitch; and

updating said estimated heading and pitch with said incremental solution.

12. The method of claim 2, wherein determining at least one of heading and pitch of the moveable platform further comprises:

receiving, from memory coupled to said computer, said initial estimate of at least one of heading and pitch of the moveable platform;

iteratively performing the computer steps of;

loading satellite ephemerides from a source coupled to said computer;

obtaining delta range measurements from each of said forward and aft positions to each of said at least two satellites;

computing estimated delta range measurements from each of said forward and aft positions to each of said at least two satellites based on said initial estimate;

comparing said obtained delta range measurements to said estimated delta range measurements;

computing a geometry matrix comprising a set of linearized range equations;

solving for an incremental estimate of at least one of heading and pitch.

13. The method of claim 12, further comprising limiting the number of iterations to a predetermined number.

14. The method of claim 12, wherein said iterative repeating comprises stopping the iterations when the solved incremental heading and pitch estimate differs from a previously solved incremental heading and pitch estimate by less than a pre-determined threshold value.

15. The method of claim 2, wherein said measuring by said first and second radar arrangements is performed between said forward-located and aft-located positions to exactly two Earth satellites.

10. A system for determining at least one of heading and pitch of a movable platform, said system comprising:

a radar arrangement mounted at forward and aft positions on said movable platform, where said forward and aft positions define a baseline, said radar arrangement being operable to measure the ranges of at least two satellites, said radar arrangement comprising;

an active radar including a first radar antenna configured to transmit a radar signal and to receive said first radar signal when said radar signal is reflected off of one of said at least two satellites, said first radar antenna mounted at said forward location; and

a passive radar receiver including a radar antenna configured to receive said radar signal transmitted by said active radar, wherein said passive radar receiver antenna is mounted at said aft location;

a computer coupled to said radar arrangement;

a memory having pre-stored therein ephemerides for said satellites, said memory coupled to said computer; and

a second memory containing estimates of heading and pitch of said moveable platform, wherein said computer is configured to set UP delta-range equations expressing a baseline vector in terms of range measurements from said forward and aft positions and said at least two satellites independently of any off-platform sensors or transmissions, and for obtaining a least squares solution for the at least one of heading and pitch using the delta-range equations and the range measurements from said forward and aft locations.

11. A system for determining at least one of heading and pitch of a movable platform, said system comprising:

a radar arrangement mounted at forward and aft positions on said movable platform, where said forward and aft positions define a baseline, said radar arrangement being operable to measure the ranges of at least two satellites, said radar arrangement comprising;

a first active radar including a first radar antenna configured to transmit a first radar signal and to receive said first radar signal when said first radar signal is reflected off of one of said at least two satellites, said first active radar antenna mounted at said forward location; and

a second active radar including a second radar antenna configured to transmit a second radar signal and to receive said second radar signal when said second radar signal is reflected off of one of said at least two satellites,

wherein said second active radar antenna is mounted at said aft location;

a computer coupled to said radar arrangement;

a memory having pre-stored therein ephemerides for said satellites, said memory coupled to said computer; and

a second memory containing estimates of heading and pitch of said moveable platform, wherein said computer is configured to set UP delta-range equations expressing a baseline vector in terms of range measurements from said forward and aft positions and said at least two satellites independently of any off-platform sensors or transmissions, and for obtaining a least squares solution for the at least one of heading and pitch using the delta-range equations and the range measurements from said forward and aft locations.

16. A system for determining heading and pitch of a movable platform, said system comprising:

a radar system located on said movable platform at one of a forward-located and an aft-located position, and also carrying a radar receiver located at the other one of said forward-located and aft-located positions, said radar system and receiver measuring the ranges to at least two Earth satellites from said radar and receiver, respectively, to form measured ranges independently of any off-platform sensors or transmissions, said radar system comprising;

an active radar including a first radar antenna configured to transmit a radar signal and to receive said radar signal when said radar signal is reflected off of one of said at least two satellites, said active radar antenna mounted at said forward location; and

a passive radar receiver including a radar antenna configured to receive said radar signal transmitted by said active radar,

wherein said passive radar receiver antenna is mounted at said aft location;

a computer coupled to said radar system and said radar receiver;

a memory having pre-stored therein satellite ephemeris data for said at least two Earth satellites, said memory coupled to said computer; and

a second memory having pre-stored therein an initial estimate of heading and pitch coupled to said computer;

wherein, said computer is configured to calculate estimated range differences between said satellites and said forward and aft locations, to form a geometry matrix from said ship-satellite geometry, to form a Jacobian matrix representing variation in said baseline vector as a function of said estimated range, to form an incremental solution for heading and pitch, and to update said estimated heading and pitch with said incremental solution.

18. The system of claim 16, wherein said measuring by said first and second radar arrangements is performed between said forward-located and aft-located positions to only two Earth satellites.

17. A system for determining heading and pitch of a movable platform, said system comprising:

a radar system located on said movable platform at one of a forward-located and an aft-located position, and also carrying a radar receiver located at the other one of said forward-located and aft-located positions, said radar system and receiver measuring the ranges to at least two Earth satellites from said radar and receiver, respectively, to form measured ranges independently of any off-platform sensors or transmissions, said radar system comprising;

a first active radar including a first radar antenna configured to transmit a first radar signal and to receive said first radar signal when said first radar signal is reflected off of one of said at least two satellites, said first active radar antenna mounted at said forward location;

a second active radar including a second radar antenna configured to transmit a second radar signal and to receive said second radar signal when said second radar signal is reflected off of one of said at least two satellites, said second active radar antenna mounted at said aft location;

a computer coupled to said radar system and said radar receiver;

a memory having pre-stored therein satellite ephemeris data for said at least two Earth satellites, said memory coupled to said computer; and

a second memory having pre-stored therein an initial estimate of heading and pitch coupled to said computer;

wherein, said computer is configured to calculate estimated range differences between said satellites and said forward and aft locations, to form a geometry matrix from said ship-satellite geometry, to form a Jacobian matrix representing variation in said baseline vector as a function of said estimated range, to form an incremental solution for heading and pitch, and to update said estimated heading and pitch with said incremental solution.