Process and device for minimizing in an inertial measurement system the error due to a perturbing motion in the retrieval of the velocity

• US 5,719,772 A
• Filed: 09/12/1995
• Issued: 02/17/1998
• Est. Priority Date: 09/28/1994
• Status: Expired due to Fees

• Current Assignee: Aerospatiale Societe Nationale Industrielle
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Benes, Christian
• Primary Examiner(s): ZANELLI, MICHAEL J
• Application Number:
  US08/526,982
• Time in Patent Office: 889 Days
• Field of Search: 364/453, 364/559, 364/571.01, 364/572
• US Class Current: 701/220
• CPC Class Codes: G01C 21/183 Compensation of inertial measurements, e.g. for temperature effects

Abstract

A process and a device are provided in a strapdown inertial measurement system for minimizing the error due to any perturbing motion in the retrieval of the velocity. The device is connected to an assembly of accelerometers and to an assembly of gyrometers and it includes a first peripheral computer for carrying out vector multiplications, a second peripheral computer for carrying out vector products, and a central computer connected to the first and second peripheral computers and coordinating the various calculations.

Claims

1. A process for minimizing, in a strapdown inertial measurement system, an error due to a perturbing motion in retrieval of a velocity, said velocity being retrieved by implementing a velocity retrieval process using measured accelerometric and gyrometric data combined with specific coefficients, said process comprising:

(a) defining an error criterion which indicates the error due to said perturbing motion in the retrieval of the velocity and which is determined from said specific coefficients;

(b) calculating, in accordance with the error criterion defined in step (a), values of said specific coefficients which enable said error criterion to be minimized; and

(c) integrating said values of the coefficients calculated in step (b) into said velocity retrieval process.

2. The process as claimed in claim 1, wherein, in order to determine velocity VF in a fixed inertial trihedron of the system, the implementation of the velocity retrieval process utilizes a velocity increment Δ

VF exhibiting a general theoretical form defined by the relation Δ

VF=B(t)Δ

Veq, in which Δ

Veq represents a velocity increment formed from said accelerometric data measured in an accelerometric trihedron moving with respect to said system, from said gyrometric data and from said specific coefficients, and B(t) is an attitude matrix depending on the time t and making it possible to transfer from the accelerometric trihedron to the inertial trihedron.

3. The process as claimed in claim 2, wherein the general theoretical form of Δ

VF is defined by the relation;

##EQU13## in which n=1, 2, . . . , p, and p is an integer greater than or equal to 2, Δ

V1 to Δ

Vp represent successive accelerometric measurements, Δ

θ

1 to Δ

θ

p represent successive gyrometric measurements, and a1 to ap as well as b1 to bp represent coefficients to be determined.

4. The process as claimed in claim 3, wherein, to determine the coefficients a1 to ap and b1 to bp:

a truncated expansion of said mean value of the velocity Δ

Vmea is carried out; and

the coefficients a1 to ap and b1 to bp which make it possible to zero at least the first order in said truncated expansion are calculated.

5. The process as claimed in claim 3, wherein, for a perturbing motion corresponding to a sculling motion consisting of a conical motion and a sinusoidal acceleration along the axis of the conical motion, a general theoretical form of Δ

VF is used for which p=2, making it possible to obtain a velocity increment defined by the relation;

space="preserve" listing-type="equation">Δ

VF=B(t) Δ

Vj+(aiΔ

θ

i+ajΔ

θ

j)Λ

(bi.DELTA.Vi+bjΔ

Vj)!

in which, for any value of ai, the coefficients aj, bi and bj satisfy;

##EQU14## with 1 a solution of the equation 1² +61-1=0, Δ

Vi and Δ

Vj being two successive accelerometric measurements and Δ

θ

i and Δ

θ

j being two successive gyrometric measurements.

6. The process as claimed in claim 3, wherein, for a perturbing motion corresponding to a sculling motion consisting of a conical motion and a sinusoidal acceleration along the axis of the conical motion, a general theoretical form of Δ

VF is used for which p=3, making it possible to obtain a velocity increment defined by the relation;

space="preserve" listing-type="equation">Δ

VF=B(t) Δ

V1+Δ

V2+Δ

V3+(a1Δ

θ

1+a2Δ

.theta.2+a3Δ

θ

3)Λ

(b1Δ

V1+b2Δ

V2+b3Δ

V3)!

in which, for any value of a3, the coefficients a1, a2, b1, b2 and b3 satisfy;

##EQU15## with k a solution of the equation;

space="preserve" listing-type="equation">6859k.sup.6 -10830k.sup.5 -6612k.sup.4 -2000k.sup.3 -348k.sup.2 -30k+1=0.

7. The process as claimed in claim 3, wherein, as error criterion, the mean value of the velocity Δ

Vmea obtained from the velocity increment Δ

VF is calculated.

8. The process as claimed in claim 2, wherein, as error criterion, the mean value of the velocity Δ

Vmea obtained from the velocity increment Δ

VF is calculated.

9. A strapdown inertial measurement system comprising:

an assembly of accelerometers for measuring accelerometric data;

an assembly of gyrometers for measuring gyrometric data; and

a device for minimizing an error due to a perturbing motion in retrieval of a velocity, said device comprising;

a first peripheral computer for carrying out vector multiplications based on the accelerometric data and the gyrometric data;

a second peripheral computer for carrying out vector products based on the accelerometric data and the gyrometric data; and

a central computer connected to said first and second peripheral computers for coordinating the vector multiplications and vector products carried out by the first and second peripheral computers to (i) define an error criterion which indicates the error due to the perturbing motion in the retrieval of the velocity and which is determined from specific coefficients, (ii) calculate, in accordance with the error criterion defined in operation (i), values of the specific coefficients which enable the error criterion to be minimized and (iii) integrating the values of the specific coefficients calculated in operation (ii) into the retrieval of the velocity.