System and method for determining an operating point

• US 5,877,723 A
• Filed: 03/05/1997
• Issued: 03/02/1999
• Est. Priority Date: 03/05/1997
• Status: Expired due to Fees

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Fan, Zhejun
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/810,798
• Time in Patent Office: 727 Days
• Field of Search: 342/357, 342/457, 701/213, 701/220, 701/216
• US Class Current: 342/357.31
• CPC Class Codes: G01S 19/49 whereby the further system is an inertial position system, e.g. loosely-coupled
• CPC Class Codes: G01S 19/53 Determining attitude

Abstract

System and method for determining an operating point of a mobile machine. The invention receives GPS information from a GPS and INU information from an inertial navigational unit. A plurality of error states are modeled. The operating point of the mobile machine is determined as a function of the error states and the GPS and INU information.

Claims

1. A method for determining an operating point of a mobile machine, including the steps of:

receiving GPS information from a GPS receiver and responsively producing a plurality of GPS signals;

receiving INU information from an inertial navigational unit and responsively producing a plurality of INU signals;

receiving the GPS and INU signals, calculating a plurality of error states as a function thereof, and responsively producing a plurality of error state signals; and

,

receiving the GPS and INU signals and the error state signals and responsively determining the operating point.

2. A method, as set forth in claim 1, wherein the step of determining the operating point is accomplished using a Kalman filter.

3. A method, as set forth in claim 1, wherein the plurality of GPS signals include GPS NORTH, GPS EAST, GPS VELOCITY NORTH, and GPS VELOCITY EAST.

4. A method, as set forth in claim 1, wherein the plurality of INU signals are used to update Kalman filter states including INU NORTH, INU EAST, INU VELOCITY, INU HEADING, and INU HEADING RATE.

5. A method, as set forth in claim 1, wherein the error state signals include BIAS RATE, RAW GPS--NORTH BIAS, and RAW GPS--E BIAS.

6. A method, as set forth in claim 1, wherein the error state signals are determined using models.

7. A method, as set forth in claim 1, wherein each error state signal is modeled using an equation of the form x(t)=Φ

₁ X(t-1)+a(t), where, x(t) represents the error state, t represents the current time, t-1 represents a previous time, a(t) represents noise, and Φ

₁ is a empirically derived constant.

8. A method, as set forth in claim 1, wherein each error state signal is modeled using an equation of the form x(t)=Φ

₁ X(t-1)+Φ

₂ X(t-2)+a(t) -Θ

₁ a(t-1), where, x(t) represents the error state, t represents the current time, t-1 and t-2 represent previous times, a(t) represents noise, and Φ

₁, Φ

₂, and Θ

₁ are empirically derived constants.

9. A system for determining an operating point for a mobile machine, comprising:

a receiver, mounted on the machine, for receiving navigation signals from a satellite-based positioning system and for responsively producing a plurality of receiver signals;

an inertial navigation unit for measuring at least one dynamic parameter of the machine and responsively producing a plurality of INU signals;

a truck reference unit for receiving the receiver and INU signals, calculating a plurality of error states as a function thereof, responsively producing a plurality of error state signals, and determining an operating point of the mobile machine as a function of the receiver and INU signals and the error state signals.