APPARATUS FOR INTEGRATING MULTIPLE RATE SYSTEMS AND METHOD OF OPERATING THE SAME

• US 20140149034A1
• Filed: 07/16/2013
• Published: 05/29/2014
• Est. Priority Date: 11/26/2012
• Status: Abandoned Application

• Current Assignee: Electronics and Telecommunications Research Institute
• Original Assignee: Electronics and Telecommunications Research Institute
• Inventors: CHO, Seong-Yun, YOON, Chang-Rak, Kim, Kyong-Ho, OH, Jae-Hong, PARK, Hye-Sun
• Application Number:
  US13/943,535
• Publication Number:
  US 20140149034A1
• Time in Patent Office: Days
• US Class Current: 701/472
• CPC Class Codes: G01C 21/165 combined with non-inertial navigation instruments

Abstract

Disclosed herein are an apparatus for integrating multiple rate systems and a method of operating an apparatus for integrating multiple rate systems. In the method of operating the apparatus, navigation information is calculated through an inertial measurement unit, and mean values and variances of initial state variables of the navigation information are set. Sigma points are calculated using the mean values and the variances. The mean values are time-propagated until measurement information is input through a Global Positioning System (GPS). When the measurement information is input, the sigma points are time-propagated at intervals of a frequency of the measurement information. Variances are calculated using the time-propagated sigma points. The navigation information is updated using the time-propagated mean values, the calculated variances, and the measurement information.

Claims

1. A method of operating an apparatus for integrating multiple rate systems, comprising:

calculating navigation information through an inertial measurement unit, and setting mean values and variances of initial state variables of the navigation information;

calculating sigma points using the mean values and the variances;

time-propagating the mean values until measurement information is input through a Global Positioning System (GPS);

when the measurement information is input, time-propagating the sigma points at intervals of a frequency of the measurement information;

calculating variances using the time-propagated sigma points; and

updating the navigation information using the time-propagated mean values, the calculated variances, and the measurement information.

2. The method of claim 1, wherein the navigation information and the measurement information are measured at frequencies for different periods.

3. The method of claim 1, wherein the navigation information includes velocity information and attitude information calculated using a 3 or more-axis gyroscope and a 3 or more-axis accelerometer.

4. The method of claim 1, wherein the measurement information includes GPS data collected using the GPS.

5. The method of claim 1, wherein time-propagating the mean values until the measurement information is input through the GPS is configured to time-propagate a mean value of a single initial state variable.

6. An apparatus for integrating multiple rate systems, comprising:

a state variable information setting unit configured to calculate navigation information using an Inertial Measurement Unit (IMU), and set mean values and variances of initial state variables of the navigation information;

a sigma point calculation unit configured to calculate sigma points using the mean values and the variances;

a time propagation unit configured to time-propagate the mean values until measurement information is input through a Global Positioning System (GPS), and when the measurement information is input, time-propagate the sigma points at intervals of a frequency of the measurement information;

an update processing unit configured to output updated navigation information in consideration of the measurement information,

wherein the state variable information setting unit calculates variances using the time-propagated sigma points, and

wherein the update processing unit updates the navigation information using the time-propagated mean values, the calculated variances, and the measurement information.

7. The apparatus of claim 6, wherein the navigation information and the measurement information are measured at frequencies for different periods.

8. The apparatus of claim 6, wherein the IMU comprises a 3 or more-axis gyroscope and a 3 or more-axis accelerometer, and collects navigation information including velocity information and attitude information using the 3 or more-axis gyroscope and the 3 or more-axis accelerometer.

9. The apparatus of claim 6, wherein the GPS collects the measurement information including GPS data.

10. The apparatus of claim 6, wherein the time propagation unit time-propagates a mean value of a single initial state variable when time-propagating the mean values.