Self-aligning pitch and azimuth reference unit

• US 4,166,406 A
• Filed: 09/06/1977
• Issued: 09/04/1979
• Est. Priority Date: 09/06/1977
• Status: Expired due to Term

• Current Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Inventors: Maughmer, Robert W.
• Primary Examiner(s): Bentley, Stephen C.
• Application Number:
  US05/830,467
• Time in Patent Office: 728 Days
• Field of Search: 73/504, 74/5.42, 74/5.44, 89/1.815, 89/41 CE, 89/41 T, 364/423, 364/424, 364/426, 364/434, 364/450, 364/453, 364/454, 364/460
• US Class Current: 89/1.815
• CPC Class Codes: F41G 5/14 for vehicle-borne guns
• CPC Class Codes: F41G 5/24 for guns on tanks
• CPC Class Codes: F41G 7/007 Preparatory measures taken before the launching of the guided missiles
• CPC Class Codes: G01C 21/166 Mechanical, construction or arrangement details of inertial navigation systems
• CPC Class Codes: G01C 21/183 Compensation of inertial measurements, e.g. for temperature effects

Abstract

A system for determining orientation or position of a movable supporting structure, such as a vehicle, includes a special inertial sensor unit. This unit includes a single gyroscope hereinafter referred to as a "gyro", with its spin axis mounted in alignment with the sensitive axis of an accelerometer. The gyro and accelerometer are mounted pendulously to rotate only about a single axis which is aligned with a direction of travel of the vehicle or with a projectile launching assembly. In additon to being pendulously mounted as mentioned above, the gyro and accelerometer combination may be rotated relative to their pendulous support, to certain fixed positions, in order to facilitate rapid initial alignment and orientation and pre-mission calibration of the inertial instruments. The pendulously mounted unit is also provided with an optical encoder to indicate the roll angle of the vehicle to which the inertial unit is secured.

In an initial rapid alignment sequence after the unit is energized, the rotation of the earth is sensed and the information stored with the unit in two or three different orientations, and, using this stored information, and the stored accelerometer outputs, the azimuth of the pendulous axis relative to true north and its pitch or elevation angle may be accurately determined.

When mounted in a vehicle and used in combination with the output from the vehicle odometer, an accurate indication of the movement of the vehicle may be obtained, and when combined with initial position and orientation data, the position of the vehicle may be continuously determined.

Claims

1. A system for determining orientation or position comprising:

movable means having a principal direction of interest;

an instrument assembly including an accelerometer having its sensitive axis aligned with said principal direction and a two-degree-of-freedom gyro having its spin axis fixedly aligned with the sensitive axis of said accelerometer; and

support means for pendulously mounting said instrument assembly to said movable means for pendulous rotation only about an axis aligned with said principal direction of interest.

2. A system as defined in claim 1 wherein said movable means is a vehicle, and wherein said principal direction of interest is the front-to-rear axis of motion of the vehicle.

3. A system as defined in claim 1 further comprising:

angular encoding means for providing an indication of the orientation of said pendulous instrument assembly relative to said movable means.

4. A system as defined in claim 1 wherein means are provided for producing first and second output signals from said gyro indicating rotation about each of two axes which are mutually orthogonal with respect to each other and with said principal direction of interest, and with one of said two axes being horizontal.

5. A system for determining orientation or position comprising:

a projectile launching assembly having a principal direction of interest in the direction in which projectiles are to be launched;

an instrument assembly including an accelerometer having its sensitive axis aligned with said principal direction and a two degree of freedom gyro having its spin axis fixedly aligned with the sensitive axis of said accelerometer; and

support means for pendulously mounting said instrument assembly to said projectile launching assembly for pendulous rotation only about an axis aligned with said principal direction of interest.

6. A system as defined in claim 5 further comprising:

a vehicle supporting said projectile launching assembly, and

means for normally supporting said projectile launching assembly with the projectile launching direction aligned with the normal front-to-rear axis of motion of said vehicle.

7. A system for determining orientation or position comprising:

movable means having a principal direction of interest;

an instrument assembly consisting solely of an accelerometer having its sensitive axis aligned with said principal direction, and a two degree of freedom gyro having its spin axis fixedly aligned with the sensitive axis of said accelerometer; and

support means for pendulously mounting said assembly to said movable means for pendulous rotation only about an axis aligned with said principal direction of interest.

9. A system as defined in claim 7 wherein said means for mechanically rotating said gyro and said accelerometer includes means for initially reversing their orientation by rotation through 180°

, and subsequently rotating to an intermediate position by rotation through 90°

if the principal direction of interest is within 45°

of true east or true west.

8. A system for determining orientation or position comprising:

movable means having a principal direction of interest;

an instrument assembly including an accelerometer having a sensitive axis and a two degree of freedom gyro having its spin axis fixedly aligned with the sensitive axis of said accelerometer;

support means for pendulously mounting said assembly to said movable means for pendulous rotation only about an axis aligned with said principal direction of interest, with the spin axis of the said gyro and the sensitive axis of the said accelerometer aligned with said principal direction of interest; and

means for mechanically rotating said gyro and accelerometer successively to a plurality of fixed discrete angular positions about an axis perpendicular to said principal direction of interest.

10. A system for determining orientation or position comprising:

a vehicle having a principal direction of interest in the direction of the front-to-rear axis of motion of said vehicle;

an instrument assembly including an accelerometer having its sensitive axis aligned with said principal direction and a two degree of freedom gyro having a spin axis fixedly aligned with the sensitive axis of said accelerometer;

support means for pendulously mounting said assembly to said movable means for pendulous rotation only about an axis aligned with said principal direction of interest;

odometer means operatively mounted in said vehicle of indicating forward movement of said vehicle; and

means for receiving data from said gyro, said accelerometer and said odometer for indicating the position of said vehicle.

11. Apparatus as recited in claim 10 in which said means for receiving data includes:

an attitude generator, including signal compensation means, connected to receive and compensate information of the angular rate about two axes normal to said principal direction from said gyro and to calculate and indicate the azimuth, elevation and roll angles of said vehicle.

12. Apparatus as recited in claim 11 in which said means for receiving data further includes:

compensation means connected to compensate the signals from said accelerometer and said odometer;

coordinate converter means connected to receive altitude signals from said attitude generator and compensated acceleration and odometer signals from said compensation means to generate coordinate converted acceleration and odometer signals; and

a present position computer connected to receive initial condition signals and said coordinate converted acceleration and odometer signals to calculate the present position of said vehicle.