Height estimating apparatus

• US 6,366,835 B1
• Filed: 05/08/2000
• Issued: 04/02/2002
• Est. Priority Date: 03/24/1999
• Status: Expired due to Fees

• Current Assignee: Atlantic Inertial Systems Incorporated (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: BAE Systems Plc
• Inventors: Henderson, Geoffrey T
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): To, Tuan C
• Application Number:
  US09/530,875
• Time in Patent Office: 694 Days
• Field of Search: 701/4, 701/3, 701/215, 701/220, 701/301, 701/2, 701/5, 701/8, 701/11, 342/462, 244/180, 244/190, 244/195
• US Class Current: 701/4
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence

Abstract

Apparatus for estimating a first height (1) of a vehicle (2) above a first reference surface (3), including a system (4) for determining position, velocity and attitude incorporating at least one sensing means (4b) operable to provide an output signal (5) indicative of a vertical specific force of the vehicle, error-estimating means (6) for receiving as input signals a horizontal reference velocity and position (4a) of the vehicle (2), and a radar altimeter measurement (7) of a second height (1b) of the vehicle (2) above a second reference surface (8) and for providing as an output signal (9) estimates of errors associated with the sensing means output signal (5), and integrating means (10) for receiving said sensing means and error-estimating means output signals (5, 9), and for subtracting the estimates of errors from the signal (5) indicative of vertical specific force while performing a double integration of the results of the subtraction, to provide an output indicative of the required estimated first height (1).

Claims

1. Apparatus for estimating a first height of a vehicle above a first reference surface, including

a system for determining position and velocity incorporating at least one sensing means operable to provide an output signal indicative of a vertical specific force of the vehicle,

error-estimating means for receiving as input signals a horizontal reference velocity and position of the vehicle, and a radar altimeter measurement of a second height of the vehicle above a second reference surface, and for providing as an output signal estimates of errors associated with the sensing means output signal, and

integrating means for receiving said sensing means and error-estimating means output signals, and for subtracting the estimates of errors from the signal indicative of vertical specific force while performing a double integration of the results of the subtraction, to provide an output indicative of the required estimated first height.

2. Apparatus according to claim 1, wherein the at least one sensing means is an inertial vertical specific force sensor operable to provide the output signal indicative of the vertical specific force of the vehicle.

3. Apparatus according to claim 1, wherein said first reference surface is sea level and said second reference surface is ground level.

4. Apparatus according to claim 3, wherein the error-estimating means includes a Kalman filter and a gravity corrector.

5. Apparatus according to claim 4, including first, second and third estimator stations at which the output signal estimates of errors associated with the sensing means output signal are stored.

6. Apparatus according to claim 5, wherein the integrating means includes first and second subtractors and first and second integrators.

7. Apparatus according to claim 6, wherein the horizontal velocity and position of the vehicle forming an input to the Kalman filter is provided by the system for determining position and velocity.

8. A method for estimating a first height of a vehicle above a first reference surface, including the steps of

operating at least one sensing means, forming part of a system for determining position and velocity of a vehicle, to provide an output signal indicative of a vertical specific force of the vehicle,

inputting a horizontal velocity and position of the vehicle and a radar altimeter measurement of a second height of the vehicle above a second reference surface to error-estimating means,

establishing in said error-estimating means estimates of errors associated with the sensing means output signal, and

subtracting the estimates of errors from the sensing means output signal while performing a double integration of the results of the subtraction, to provide the required estimated first height.

9. A method according to claim 8, in which said double integration includes a first integration, which first integration integrates the vertical specific force to provide a vertical velocity, and a second integration, which second integration integrates the vertical velocity in order to provide the required estimated first height.

10. A method according to claim 9, in which the at least one sensing means is a vertical specific force sensor, with estimates of a bias associated with the vertical specific force sensor being provided by a Kalman filter, together with estimates of a vertical velocity error and estimates of a vertical height error associated with the system for determining position and velocity.

11. A method according to claim 10, in which said subtraction of estimates of errors includes a first subtraction, which first subtraction is effected while performing the first integration and subtracts the estimate of the bias associated with the specific force sensor and a correction for gravity supplied by the gravity corrector from said vertical specific force on a continuous basis, together with a subtraction of the vertical velocity error at discrete intervals, and a second subtraction, which second subtraction is effected on the second integration at discrete intervals and subtracts the vertical height error estimate therefrom to provide the required estimated first height.

12. A method according to claim 11, in which the double integration is effected at a processing cycle frequency of substantially 50 Hz and outputs the required estimated first height at an output rate of substantially 50 Hz, the radar altimeter measurement of a second height of the vehicle above a second reference surface is input to the estimating means at an input rate of substantially 12.5 Hz, and in which the estimate of the bias of the vertical specific force sensor, the estimate of gravity, the vertical velocity error estimate and the vertical height error estimate are used to correct the double integration with a correction cycle frequency in the range of from 2 to 4 Hz.