Inertial navigation system

• US 4,085,440 A
• Filed: 05/05/1977
• Issued: 04/18/1978
• Est. Priority Date: 05/05/1977
• Status: Expired due to Term

• Current Assignee: United States Of America As Represented By The Secretary Of The Army (Government of the United States of America)
• Original Assignee: The United States Of America As Represented By The Secretary Of The Army
• Inventors: Hose, Eddy
• Primary Examiner(s): Gruber, Felix D.
• Application Number:
  US05/794,195
• Time in Patent Office: 348 Days
• Field of Search: 235/150.2, 235/24, 235/25, 235/27, 235/271, 73/178, 73/382
• US Class Current: 701/221
• CPC Class Codes: G01C 21/18 Stabilised platforms, e.g. by gyroscope
• CPC Class Codes: G06G 7/78 for direction-finding, locating, distance or velocity measuring, or navigation systems

Abstract

A navigational system for automatically positioning a platform relative to the earth'"'"'s geopotential surface. A system is provided which includes an accurate self-contained attitude reference to the true vertical. The system includes an inertial platform which is rotatable relative to a level platform, each of the platforms being connected to a two axis gimbal. One of the platforms is also connected to a three axis gimbal which may be connected to the vehicle which it is desired to stabilize. Means are provided for sensing rotation of one platform relative to the other. An inertial platform position control computer is provided for generating first corrected signals to the three axis gimbal for automatically referencing the inertial platform to a datum reference spheroid. Additional computer means are provided for generating second corrected signals to the two axis gimbal to align the level platform with the true vertical to the geopotential surface of the earth.

Claims

1. A navigational system comprising:

a platform assembly comprising an inertial platform unit which includes an inertial platform, a level platform unit which comprises a level platform, said inertial platform and said level platform being connected to a two axis gimbal, said inertial platform being rotatable relative to said level platform, and means connected to said two axis gimbal for sensing said rotation,

a three axis gimbal connected to said platform assembly for referencing said inertial platform in response to first corrected signals and for connecting said assembly to a vehicle,

an inertial platform position control computer for generating said first corrected signals to said three axis gimbal, in response to first output signals generated from a control means to said inertial platform unit and first positioning signals received from said inertial platform unit, for referencing said inertial platform to a datum reference spheroid, and,

a control means for generating said first output signals, and for generating second corrected signals to said two axis gimbal in response to second positioning signals received from said level platform unit, second output signals received from said sensing means, and third output signals received from said inertial platform unit, for aligning said level platform with the true vertical to the geopotential surface of the earth.

2. The system of claim 1 wherein said sensing means comprises a noth transducer and an east transducer for sensing the level error in the north and east directions, respectively, and for producing said second output signals, which comprise respective north and east transducer signals, corresponding to said sensed error, and emitting said signals to said control means.

3. The system of claim 2 wherein said level platform unit comprises an orthogonal vertical north rotating gravity gradiometer and an orthogonal vertical east rotating gravity gradiometer aligned with the north and east axes, respectively, said gradiometers producing said second positioning signals which comprise respective north gradiometer signals and east gradiometer signals, and emitting said signals to said control means.

4. The system of claim 3 wherein said inertial platform unit comprises an orthogonally oriented north accelerometer and an orthogonally oriented east accelerometer aligned with the north and east axes, respectively, said accelerometers producing said third output signals which comprise respective north and east acceleration signals, and emitting said signals to said control means.

5. The system of claim 4 wherein said inertial platform unit further comprises an orthogonally mounted north gyroscope and an orthogonally mounted east gyroscope, aligned with the north and east axes, respectively, and gyroscopes receiving said first output signals from said control means, resolving said first output signals into said first positioning signals which comprise north and east positioning signals, respectively, and emitting said north and east positioning signals to said inertial platform position control computer.

6. The system of claim 5 wherein said control means comprises:

a navigational computer for receiving said acceleration and transducer signals, resolving said acceleration and transducer signals into corrected acceleration signals, and emitting said corrected signals to a leveling computer, said leveling computer also receiving said transducer and second positioning signals, resolving said corrected acceleration, transducer and second positioning signals into drive signals, and

means for resolving said drive signals into said second corrected signals.

7. The system of claim 6 wherein said resolving means comprises north and east servomechanisms

8. The system of claim 7 wherein said three axis gimbal is connected to said level platform.

9. A navigational system comprising:

a platform assembly comprising an inertial platform and a level platform connected to a two axis gimbal, said inertial platform being rotatable relative to said level platform;

a three axis gimbal connected to said platform assembly;

north and east transducers connected to said two axis gimbal for sensing the level error in the north and east directions, respectively, and producing respective north and east transducer signals corresponding to said sensed error;

north and east orthogonal vertical rotating gravity gradiometers connected to said level platform and aligned with said platform'"'"'s north and east axes, respectively, for producing respective north and east gradiometer signals;

north and east orthogonally oriented accelerometers connected to said inertial platform and aligned with said platform'"'"'s north and east axes, respectively, for producing respective north and east acceleration signals;

a navigational computer for producing first output signals, and for receiving said acceleration and transducer signals, and resolving said acceleration and transducer signals into corrected acceleration signals;

north and east orthogonally mounted gyroscopes connected to said inertial platform and aligned with said platform'"'"'s north and east axes, respectively, for receiving said first output signals from said navigational computer, and resolving said first output signals into respective north and east positioning signals;

a leveling computer for receiving corrected acceleration, transducer and gradiometer signals, and resolving said corrected acceleration, transducer and gradiometer signals into drive signals;

an inertial platform position control computer for receiving said north and east positioning signals, and further positioning signals produced by said inertial platform, resolving said positioning signals into first corrected signals, and emitting said first corrected signals to said three axis gimbal for referencing said inertial platform to a datum reference spheroid; and

,

north and east servo mechanisms for receiving said drive signals, resolving said drive signals into second corrected signals and emitting said second corrected signals to said two axis gimbal for aligning said level platform with the true vertical to the geopotential surface of the earth.

10. The system of claim 9 wherein said three axis gimbal is connected to said level platform.