Automatic sensor alignment

• US 5,245,909 A
• Filed: 05/07/1990
• Issued: 09/21/1993
• Est. Priority Date: 05/07/1990
• Status: Expired due to Fees

• Current Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Original Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Inventors: Berg, Robert L., Corrigan, John D., Simmons, Dennis E. Jr.
• Primary Examiner(s): Jordan, Charles T.
• Application Number:
  US07/520,272
• Time in Patent Office: 1,233 Days
• Field of Search: 244/3.1, 89/41.19, 89/41.21
• US Class Current: 89/41.19
• CPC Class Codes: F41G 1/54 Devices for testing or checking ; Tools for adjustment of sights
• CPC Class Codes: F41G 3/326 for checking the angle between the axis of the gun sighting device and an auxiliary measuring device F41G3/323 takes precedence
• CPC Class Codes: G01C 21/183 Compensation of inertial measurements, e.g. for temperature effects
• CPC Class Codes: G01C 25/005 initial alignment, calibration or starting-up of inertial devices

Abstract

A problem faced by designers of advanced electronic military equipment is the strigent angular alignment requirement of aircraft avionics and weapon system sensors. Meeting the alignment requirements in the case of advanced systems presents an ever-increasing problem. In airborne systems, as the alignment requirements of its sensors are becoming more stringent, the aircraft are becoming more flexible structurally. Conventional sensor alignment systems are expensive and utilize complex optical-mechanical equipment and procedures, for instance aircraft jacks, optical targeting boards, precision optical mirrors, sophisticated tooling, and ground support personnel. Past alignment procedures also required ground personnel having the same skill level as those in the aircraft in order to operate such equipment as optical target boards, precision optical mirrors, autocollimators and other instruments. By of this invention a system for aligning avionic/weapon sensors is provided which eliminates the need for support equipment outside the vehicle to boresight and align sensors on the the vehicle. It also allows more flexibility in the location of alignment-sensitive equipment when the vehicle, especially aircraft, is designed.

Claims

1. An aligning system for maintaining precise alignment of alignment-sensitive guidance and avionics sensing instruments in moving vehicles comprising a plurality of alignment modules, each mounted on, and in alignment with, an initially precisely aligned sensing instrument, each alignment module including an accelerometer triad which is adapted to define an orthogonal coordinate system for sensing instrument orientation in three dimensions, and to generate specific force vectors in that coordinate system, a reference module including three accelerometers which are adapted to define a fixed orthogonal vehicle body coordinate system, and to generate specific force vectors relative to that coordinate system, means for continuously determining from the specific force vectors misalignment angles between alignment modules and the reference module, and for ascertaining a transformation accomplishing alignment, and means effecting the transformation to correct for said misalignment.

2. The aligning system of claim 1 wherein a Kalman filter is included for comparing acceleration outputs.

3. The aligning system of claim 1 wherein the alignment accelerometer module is integrated with a forward looking infrared sensing device.

4. The aligning system of claim 1 wherein the reference accelerometer module is integrated with an inertial navigation system.

5. The aligning system of claim 1 wherein the vehicle is a ship.

6. The aligning system of claim 1 wherein the vehicle is a tank.

7. The aligning system of claim 1 wherein the vehicle is an aircraft.

8. The aligning system of claim 7 wherein the reference module is the aircraft'"'"'s strapdown inertial navigation system.

9. The aligning system of claim 1 wherein the vehicle is a missile.

10. The aligning system of claim 1 wherein at least part of the alignment system is in a weapon.

11. A process for aligning alignment-sensitive weapons and avionics sensors which are subject to misalignment during use which comprises measuring specific force vectors in a first accelerometer in an orthogonal coordinate system whose vertical and horizontal axes correspond to the sensor axes, measuring specific force vectors in a second accelerometer in a reference orthogonal coordinate system corresponding to the aircraft body, continuously determining from the specific force vectors misalignment angles between the first coordinate system and the reference coordinate system, ascertaining a transformation accomplishing alignment, and effecting the transformation to correct for said misalignment.

12. The aligning process of claim 11 wherein at least one of the alignment steps is in a weapon.