Passive navigation system

• US 5,912,643 A
• Filed: 05/29/1997
• Issued: 06/15/1999
• Est. Priority Date: 05/29/1997
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Ritchie, Henry F, Dmytrasz, Joseph N., Sumner, Donald L., Gatta, Joseph, Chew, Sung-Leung
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/865,541
• Time in Patent Office: 747 Days
• Field of Search: 342/357, 342/457, 701/214, 701/216, 701/221, 701/224
• US Class Current: 342/457
• CPC Class Codes: G01C 21/185 for gravity
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems

Abstract

A Passive Navigation System (PNS) provides continuous updating of position, velocity, and attitude information of a vehicle without recourse to radiating or external navigation aids. The system accurately computes navigation information with the utilization of gravity sensors, gravimetric maps, vertical position, and velocity measurements. Sensor and map data are optimally processed by real time filtering to compute the best position, velocity, and attitude of the vehicle. The products of measured gravity gradients and the velocity of the vehicle are integrated over time to obtain a north, east, down gravity vector components which are combined with corresponding components obtained from a vertical deflection map in a complementary filter. North and east components of the combination are compared with the corresponding components from the vertical deflection map, while the down component of the gravity is compared to the down value obtained from a gravimeter. Residuals from these comparisons are utilized in a Kalman filter to provide corrections that render inertial measuring units in the system independent of the vertical deflections and gravity anomalies. Measured gravity gradients are compared to reference map gradients, the residuals being utilized in the kalman filter to estimate long term position errors and to provide correction for gradiometer bias and drift. A vertical position loop mixes gravity down data obtained from a gravimeter and gravity down data obtained from the integrator to provide vertical position which is compared to a reference derived from the difference between a measured vehicle height and terrain height obtained from a geoidal map. The residual of this comparison is utilized in the Kalman filter to improve estimates of east velocity.

Claims

1. An apparatus for navigating a vehicle, of the type having gravity measuring means for determining gravitational fields, gradiometer means for determining gravity gradients, gravity reference map means for providing reference gravity data, means for providing vehicle position and velocity, and a Kalman filter which utilizes the data supplied to provide a state vector, the components of which are used to update the various sensors of the navigation apparatus comprising:

an integrator coupled to receive signals representative of vehicle velocity from said position and velocity means and signals representative of gravity gradient from said gradiometer means for providing signals representative of an integration over a selected time interval of a product of said gravity gradient and said vehicle velocity, thereby providing output signals representative of a gravity vector having a gravity north component, a gravity east component, and a gravity down component;

a complementary filter coupled to receive signals representative of gravity north and gravity east components from said reference map means and said gravity north and gravity east component representative signals from said integrator to provide signals representative of gravity vertical deflection;

first differencing means coupled to receive said signals representative of gravity vertical deflection from said complementary filter and signals representative of gravity vertical deflection from said gravity reference map means for coupling signals representative of differences between gravity vertical deflection provided by said gravity reference map means and gravity vertical deflection provided by said complementary filter to said Kalman filter, wherein a state vector is determined and an output terminal; and

means coupled to receive said state vector for updating position, velocity, and attitude of said vehicle.

2. The navigation apparatus of claim 1 further comprising vertical deflection speed corrector means coupled between said first differencing means said Kalman filter said speed corrector means further coupled to receive signals representative of vehicle speed from said position and velocity means for providing speed corrections to said vertical deflection difference representative signals.

3. The navigation apparatus of claim 2 further comprising second differencing-means coupled to said gravity means for receiving signals representative of measured gravity down components and to said integrator for receiving said gravity down representative signals for providing signals representative of differences between said gravity down components and said measured gravity down components, said differences between said gravity down components and said measured gravity down components coupled to said Kalman filter for providing east velocity correction components in said state vector.

4. The navigation apparatus of claim 3 further comprising:

vertical position means coupled to receive said signal representative of said difference between said down component and said measured down component for providing a signal representative of vertical position of said vehicle;

sensor means for providing signals representative of vehicle vertical position;

geoidal height map means for providing signals representative of terrain height;

third differencing means coupled to receive said vehicle vertical position representative signals and said terrain height representative signals for providing vertical difference signals representative of differences between said vehicle vertical position and said terrain height;

fourth differencing means coupled to receive said vertical position representative signals and said vertical difference representative signals for providing difference signals representative of differences between said vertical position representative signals and said vertical difference representative signals at an output terminal coupled to said Kalman filter for providing a second east velocity correction component in said state vector.

5. The navigation apparatus of claim 4 wherein said gradiometer means provides a measured gravity gradient matrix and said gravity reference means provides a reference gravity gradient matrix and further comprising second differencing means coupled to said gradiometer means and said gravity map means for providing signals respectively representative of differences between corresponding components of said measured gravity matrix and said reference gravity gradient matrix, said second difference means having output terminals coupled to said Kalman filter for providing signals representative of long term position errors and signals for correcting gradiometer bias and drift.

6. The navigation apparatus of claim 1 wherein said gradiometer means provides a measured gravity gradient matrix and said gravity reference map means provides a reference gravity gradient matrix and further comprising second differencing means coupled to said gradiometer means and said gravity reference map means for providing signals respectively representative of differences between corresponding components of said measured gravity matrix and said reference gravity gradient matrix at output terminals coupled to said Kalman filter for providing signals representative of long term position errors and signals for correcting gradiometer bias and drift.

7. The navigation apparatus of claim 1 wherein said reference map means provides signals representative of reference gravity anomalies and said gravity measuring means provides signals representative of measured gravity anomalies and further comprising second differencing means coupled to said reference map means and said gravity measuring means for providing a signal representative of a difference between said measured gravity anomalies and said reference gravity anomalies, said second difference means having an output port coupled to said Kalman filter for providing signals representative of vehicle position errors.

8. The navigation apparatus of claim 1 further comprising second differencing means coupled to said gravity means for receiving signals representative of measured gravity down components and to said integrator for receiving said gravity down component representative signals to provide signals representative of differences between said gravity down component representative signals and said measured down component representative signals, said differences between said gravity down component representative signals and said measured gravity down component representative signals coupled to said Kalman filter for providing east velocity correction components in said state vector.

9. An apparatus for navigating a vehicle, of the type having gravity measuring means for determining gravitational fields, gradiometer means for determining gravity gradients, gravity reference map means for providing gravity data, means for providing vehicle position and velocity, and a Kalman filter which utilizes the data supplied to provide a state vector, the components of which are used to update the various sensors of the navigation apparatus comprising:

an integrator coupled to receive signals representative of vehicle velocity from said position and velocity means and signals representative of gravity gradient from said gradiometer means for providing a signal representative of an integration over a selected time interval of a product of said gravity gradient and said vehicle velocity, thereby providing output signals representative of a gravity vector having a gravity north component, a gravity east component, and a gravity down component;

first differencing means coupled to said gravity measuring means for receiving a signal representative of a measured down component of gravity and to said integrator for receiving said output signal representative of said down component of gravity to provide a signal representative of a difference between said down component of gravity and said measured down component of gravity;

vertical position means coupled to receive said signal representative of said difference between said down and said measured down components of gravity for providing a vertical position correction signal;

sensor means for providing a signal representative of vehicle vertical position;

geoidal height map means for providing a signal representative of terrain height;

second differencing means coupled to receive said vehicle vertical position representative signal and said terrain height representative signal for providing a vertical position difference signal representative of a difference of said vehicle vertical position and said terrain height;

third differencing means coupled to receive said vertical position correction signal and said vertical difference representative signal for providing a difference signal representative of a difference between said vertical position correction signal and said vertical difference representative signal to said Kalman filter from which an east velocity correction component in said state vector is determined.

10. An apparatus for navigating a vehicle, the apparatus being of the type having gravity measuring means for determining gravitational fields, gradiometer means for determining gravity gradients, gravity reference map means for providing gravity data, means for providing vehicle position and velocity, and a Kalman filter which utilizes the data supplied to provide a state vector, the components of which are used to update the various sensors of the navigation apparatus characterized in that:

said gradiometer means provides a measured gravity gradient matrix and said gravity reference means provides a reference gravity gradient matrix; and

in that said apparatus further comprises

first differencing means coupled to said gradiometer means and said gravity reference map means for providing signals respectively representative of differences between corresponding components of said measured gravity matrix and said reference gravity gradient matrix, said first difference means having output terminals coupled to said Kalman filter for providing signals representative of long term position errors and signals for correcting gradiometer bias and drift,

an integrator coupled to receive signals representative of vehicle velocity from said velocity means and signals representative of gravity gradient from said gradiometer means for providing signals representative of an integration over a selected time interval of a product of said gravity gradient and said vehicle velocity, thereby providing output signals representative of a gravity vector having a gravity north component, a gravity east component, and a gravity down component;

second differencing means coupled to said gravity means for receiving signals representative of measured gravity down component and to said integrator for receiving signals representative of gravity down component for providing signals representative of differences between said gravity down component and said measured gravity down component;

vertical position means coupled to receive said signals representative of said differences between said gravity down component and said measured gravity down component for providing vertical position signals representative of vertical positions of said vehicle;

sensor means for providing signals representative of vehicle vertical positions;

geoidal height map means for providing signals representative of terrain heights;

third differencing means coupled to receive said vehicle vertical position representative signals and said terrain height representative signals for providing vertical difference signals representative of differences of said vehicle vertical positions and said terrain heights;

fourth differencing means coupled to receive said vertical position representative signals and said vertical difference representative signals for providing difference signals representative of differences between said vertical position representative signals and said vertical difference representative signals to said Kalman filter from which an east velocity correction component in said state vector is determined.