Remote alignment system

• US 5,729,234 A
• Filed: 09/23/1996
• Issued: 03/17/1998
• Est. Priority Date: 09/23/1996
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Patel, Naresh Raman, Morris, Randall Deen, Stetson, John Batterson Jr.
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US08/717,962
• Time in Patent Office: 540 Days
• Field of Search: 342/59, 342/125, 342/126, 342/139, 342/140, 342/146, 342/147, 342/463, 342/62, 342/63
• US Class Current: 342/62
• CPC Class Codes: F41G 7/2206 using a remote control station
• CPC Class Codes: F41G 7/226 Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
• CPC Class Codes: F41G 7/2286 using radio waves
• CPC Class Codes: G01C 25/005 initial alignment, calibration or starting-up of inertial devices
• 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 2205/005 for aircraft positioning relative to other aircraft
• CPC Class Codes: G01S 5/0036 of measured values, i.e. measurement on mobile and position calculation on base station
• CPC Class Codes: G01S 7/003 Transmission of data between radar, sonar or lidar systems and remote stations
• CPC Class Codes: G01S 7/4091 during normal radar operation
• CPC Class Codes: G01S 7/497 Means for monitoring or calibrating

Abstract

An arrangement for coordinating positional and angle information made on separate relatively moving platforms, such as aircraft, having independent coordinate systems, uses measurements of a common reference made on both platforms. The measurements are transmitted to a common location. Measurements made at a first time are processed to determine two of three coordinate transformation angles. After a period of time, a second set of measurements is used to determine the third coordinate transformation angle. In a particular embodiment of the invention, the direction of motion of one of the platforms is controlled to be orthogonal to a coordinate axis of the other platform. When the coordinate transformation is determined, it can be used to coordinate or align navigation instruments, weapons, or the like. In one embodiment of the invention, a missile is directed toward a target, in a situation in which the target is viewed from the missile and another moving vehicle.

Claims

1. An apparatus for determining the attitude of a relatively moving object from first and second position measurements made at itself and at another object, said apparatus comprising:

a first object having a first coordinate system including mutually orthogonal x,y and z coordinate axes;

a second object, remote from said first object, and which may be in compound motion relative thereto, said second object having a second coordinate system including mutually orthogonal r,s and t coordinate axes, which may not correspond with said first coordinate system;

a reference object displaced from both said first and second objects;

signal generating means coupled to said first, second, and reference objects for generating, first and second position signals representative of the position of said reference object relative to said first and second objects, respectively, and a third position signal representative of the position of said second object relative to said first object at a first instant of time, and for generating fourth and fifth position signals representative of the position of said reference object relative to said first and second objects, respectively, at a second instant of time at which said second object is at a different position relative to said first object than at said first instant, and a sixth position signal representative of the position of said second object relative to said first object, said first, third, fourth and sixth position signals being measured in said first coordinate system, and said second and fifth position signals being measured in said second coordinate system, and;

processing means coupled to said signal generating means for estimating the position of said second object relative to said reference object based upon said first and third reference signals, and for comparing said estimate of said position of said second object relative to said reference object with said second position signal for generating first and second angles of a three-angle transformation matrix representative of the attitude of said second coordinate system relative to said first coordinate system, and for estimating said third angle of said transformation matrix from said fourth, fifth, and sixth position signals.

2. A method for directing a first vehicle from a second vehicle, where the coordinate systems of the two vehicles are relatively skewed, said method comprising the steps of:

measuring the direction and range of a reference object from said first and second vehicles, to produce first and second signals, respectively, representing the direction and range of said reference object in first and second coordinate systems associated with said first and second vehicles, respectively;

measuring the direction and range of said first vehicle from said second vehicle, to generate third signals representing the range and position of said first vehicle in said second coordinate system;

transmitting said first signals from said first vehicle to said second vehicle;

at said second vehicle, estimating said direction and range from said first vehicle to said reference object based upon said first and second measurements made in said second coordinate system, to produce estimated first signals;

at said second vehicle, determining two of three components of a coordinate transformation between said first and second coordinate systems from said first signal and said estimated first signal;

repeating said steps of (a) measuring the direction and range of a reference object from said first and second vehicles, (b) measuring the direction and range of said first vehicle from said second vehicle, (c) measuring the direction and range of said first vehicle from said second vehicle, (d) transmitting said first signals from said first vehicle to said second vehicle, and (e) estimating said direction and range from said first vehicle to said reference object based upon said first and second measurements made in said second coordinate system, to form later measurements;

at said second vehicle, determining from the combination of said first signals, estimated first signals, and said later measurements, the third component component of said coordinate transformation.

3. A method according to claim 2 further comprising the step of:

before said step of repeating said steps of (a), (b), (c), (d) and (e), directing said first vehicle in a direction orthogonal to an axis of said second coordinate system.