Vehicle dynamics conditioning method on MEMS based integrated INS/GPS vehicle navigation system

• US 20080071476A1
• Filed: 09/19/2006
• Published: 03/20/2008
• Est. Priority Date: 09/19/2006
• Status: Abandoned Application

• Current Assignee: Alpine Electronics Incorporated (Alps Alpine Co., Ltd.)
• Original Assignee: Alpine Electronics Incorporated (Alps Alpine Co., Ltd.)
• Inventors: Hoshizaki, Takayuki
• Application Number:
  US11/523,127
• Publication Number:
  US 20080071476A1
• Time in Patent Office: Days
• US Class Current: 701/214
• CPC Class Codes: G01C 21/165 combined with non-inertial navigation instruments
• CPC Class Codes: G01S 19/26 involving a sensor measurement for aiding acquisition or tracking
• CPC Class Codes: G01S 19/49 whereby the further system is an inertial position system, e.g. loosely-coupled

Abstract

A method of compensating performance of low-cost MEMS (microelectro mechanical systems) inertial sensors in an integrated INS/GPS navigation system for automotive application is disclosed. The proposed method includes velocity and inertial sensor output conditions featured in ground vehicle dynamics. Using the conventional Kalman filter based INS/GPS system, implementation of the prescribed conditions in the present invention additionally to the GPS measurements shows accurate motion tracking even when GPS signal dropouts last for more than 2 minutes. Another aspect of the disclosure is an integrated INS/GPS navigation system which utilizes MEMS based inertial sensors for maintaining high position tracking accuracy even when a GPS signal is lost or unavailable for a long period of time by incorporating the predefined vehicle dynamics conditions when calculating optimum estimates through the Kalman filtering process.

Claims

1. A navigation method of conditioning ground vehicle'"'"'s dynamics for microelectro mechanical system (MEMS) based integrated inertial navigation system (INS)/GPS navigation systems, comprising the steps of:

(a) defining vehicle dynamics conditions in advance as a function of accelerations and angular rates obtained from inertial sensors;

(b) receiving the accelerations and angular rates corresponding to coordinates of a ground vehicle from inertial sensors mounted on the INS;

(c) detecting a current dynamics condition of the vehicle by evaluating the accelerations and angular rates from the inertial sensor;

(d) sending measured data indicative of the detected vehicle dynamics condition to a Kalman filter which integrates the INS and GPS to conduct a Kalman filter processing incorporating the vehicle dynamics condition; and

(e) repeating the steps (b) to (d) to obtain optimum estimates of current vehicle position, velocity and orientation.

2. The navigation method as defined in claim 1, wherein one of said vehicle dynamics conditions is a normal condition wherein lateral and downward velocities are assumed to be zero in terms of a vehicle-fixed coordinate system.

3. The navigation method as defined in claim 1, wherein one of said vehicle dynamics conditions is a cornering condition wherein a forward velocity is estimated from a lateral acceleration and a directional angular rate, and a lateral velocity is assumed to be a small value, and a downward velocity is assumed to be zero, in terms of a vehicle-fixed coordinate system.

4. The navigation method as defined in claim 1, wherein one of said vehicle dynamics conditions is a stationary condition wherein a vehicle'"'"'s all three coordinate velocities are assumed to be zero after detecting a stopping status.

5. The navigation method as defined in claim 1, wherein the inertial sensors are configured by three-axis accelerometers and three-axis gyroscopes in which accelerations corresponding to coordinates of the vehicle are detected by the three accelerometers and the angular rates corresponding to coordinate directions of the vehicle are detected by the three gyroscopes.

6. The navigation method as defined in claim 3, wherein the forward velocity of the vehicle in the cornering condition is estimated by a lateral acceleration and a directional angular rate of the vehicle when the vehicle is cornering.

7. The navigation method as defined in claim 4, wherein the inertial sensors are configured by three accelerometers and three gyroscopes in which the inertial sensors are configured by three accelerometers and three gyroscopes in which outputs of the gyroscopes are assumed to be zero in the stationary condition.

8. The navigation method as defined in claim 1, wherein said measured data indicative of the detected vehicle dynamics condition is sent to the Kalman filter at a rate higher than that of a GPS output which is indicative of absolute location and velocity of the vehicle.

9. The navigation method as defined in claim 8, wherein said measured data indicative of the detected vehicle dynamics condition is sent to the Kalman filter at a rate of 10 Hz and the GPS output indicative of the absolute location and velocity of the vehicle is sent to the Kalman filter at a rate of 1 Hz.

10. An integrated INS (inertial navigation system)/GPS (global positioning system) navigation system implementing microelectro mechanical system (MEMS) sensors for a ground vehicle, comprising:

an inertial navigation system (INS) having an inertial measurement unit (IMU) which incorporates MEMS sensors;

a GPS (global positioning system) receiver which receives satellite signals from a plurality of satellites to produce GPS measurements indicating absolute position and velocity of the ground vehicle;

a Kalman filter which combines outputs of the INS and the GPS receiver and performs a Kalman filter processing; and

a vehicle dynamics conditioning (VDC) controller which controls an overall operation of the navigation system including vehicle dynamics conditions detected from output of the MEMS sensors;

wherein said vehicle dynamics conditions include a normal condition, a cornering condition and a stationary condition of the ground vehicle.

11. The integrated INS/GPS navigation system as defined in claim 10, wherein said MEMS sensors are configured by three-axis accelerometers and three-axis gyroscopes in which accelerations corresponding to coordinates of the vehicle are detected by the three-axis accelerometers and the angular rates corresponding to coordinate directions of the vehicle are detected by the three-axis gyroscopes.

12. The integrated INS/GPS navigation system as defined in claim 10, wherein one of said vehicle dynamics conditions is a normal condition wherein lateral and downward velocities are assumed to be zero in terms of a vehicle-fixed coordinate system.

13. The integrated INS/GPS navigation system as defined in claim 10, wherein one of said vehicle dynamics conditions is a cornering condition wherein a forward velocity is estimated from a lateral acceleration and a directional angular rate, and a lateral velocity is assumed to be a small value, and a downward velocity is assumed to be zero, in terms of a vehicle-fixed coordinate system.

14. The integrated INS/GPS navigation system as defined in claim 10, wherein one of said vehicle dynamics conditions is a stationary condition wherein a vehicle'"'"'s all three coordinate velocities are assumed to be zero after detecting a stopping status.

15. An integrated INS (inertial navigation system)/GPS (global positioning system) navigation system implementing microelectro mechanical system (MEMS) sensors for a ground vehicle, comprising

means for defining vehicle dynamics conditions in advance as a function of accelerations and angular rates obtained from inertial sensors;

means for receiving the accelerations and angular rates corresponding to coordinates of a ground vehicle from inertial sensors mounted on the INS;

means for detecting a current dynamics condition of the vehicle by evaluating the accelerations and angular rates from the inertial sensor;

means for sending measured data indicative of the detected vehicle dynamics condition to a Kalman filter which integrates the INS and GPS to conduct a Kalman filter processing incorporating the vehicle dynamics condition; and

means for repeating the steps (b) to (d) to obtain optimum estimates of current vehicle position, velocity and orientation.

16. The integrated INS/GPS navigation system as defined in claim 15, wherein one of said vehicle dynamics conditions is a normal condition wherein lateral and downward velocities are assumed to be zero in terms of a vehicle-fixed coordinate system.

17. The integrated INS/GPS navigation system as defined in claim 15, wherein one of said vehicle dynamics conditions is a cornering condition wherein a forward velocity is estimated from a lateral acceleration and a directional angular rate, and a lateral velocity is assumed to be a small value, and a downward velocity is assumed to be zero, in terms of a vehicle-fixed coordinate system.

18. The integrated INS/GPS navigation system as defined in claim 15, wherein one of said vehicle dynamics conditions is a stationary condition wherein a vehicle'"'"'s all three coordinate velocities are assumed to be zero after detecting a stopping status.

19. The integrated INS/GPS navigation system defined in claim 15, wherein the inertial sensors are configured by three-axis accelerometers and three-axis gyroscopes in which accelerations corresponding to coordinates of the vehicle are detected by the three-axis accelerometers and the angular rates corresponding to coordinate directions of the vehicle are detected by the three-axis gyroscopes.

20. The integrated INS/GPS navigation system navigation method as defined in claim 17, wherein the forward velocity of the vehicle in the cornering condition is estimated by a lateral acceleration and a directional angular rate of the vehicle when the vehicle is cornering.