Navigation method

• US 4,809,007 A
• Filed: 03/02/1987
• Issued: 02/28/1989
• Est. Priority Date: 03/03/1986
• Status: Expired due to Fees

• Current Assignee: Litef GmbH Lorracher STR
• Original Assignee: Litef GmbH (Northrop Grumman Corporation)
• Inventors: Hassenplug, Wolfgang
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US07/020,851
• Time in Patent Office: 729 Days
• Field of Search: 342/417, 342/448, 364/453, 244/3.2
• US Class Current: 342/417
• CPC Class Codes: G01C 19/36 with north-seeking action by magnetic means, e.g. gyromagnetic compasses

Abstract

A navigation method for independently determining direction and for determining course for aircraft with low quality gyros and an external, calibrated magnetic course sensor. The method, which functions in the event of failure of the magnetic course sensor, is based upon the concept of determining, from the magnetic course last determined prior to failure as corrected by the local declination, and the true course as determined by the quotient of the two gyro horizontal axes distorted by the gyro drift, a "synthetic magnetic course" for course support.

Claims

1. A method for determining the course of an aircraft of the type that includes at least one gyro and an external calibrated magnetic course sensor in the event of failure of said magnetic course snsor, said method comprising the steps of:

(a) measuring true north course by means of said magnetic sensor; and

(b) measuring local magnetic variation;

then

(c) correcting said true north course by combining said magnetic variation with said measured true north course; and

(d) determining the differential angle from gyro drift, the earth'"'"'s rotation and latitude; and

(e) independently continuously determining course angle ψ

_A from said corrected true north course and said differential angle;

then

(f) storing said independent course angle; and

then;

(g) calculating true north course by correcting said independent course with, the differential angle determined prior to failure of said magnetic course sensor.

2. A method as defined in claim 1 wherein said magnetic sensor is a calibrated three-axis magnetometer.

3. A method as defined in claim 1 wherein said magnetic sensor is a calibrated flux valve.

4. A method as defined in claim 1 further including the steps of:

(a) calculating said correction differential angle by averaging a plurality of values of said differential angle δ

ψ

over a predetermined period of time;

then

(b) extrapolating said averaged differential angle corrected according to instantaneous latitude.

5. A method as defined in claim 1 further including the step of compensating the speed-dependent errors of said independent course determination by means of a speed reference.

6. A method as defined in claim 5 wherein said speed reference is a Doppler radar.