Global positioning system (GPS) Compass

• US 5,777,578 A
• Filed: 02/10/1997
• Issued: 07/07/1998
• Est. Priority Date: 02/10/1997
• Status: Expired due to Term

• Current Assignee: National Science Council
• Original Assignee: National Science Council
• Inventors: Wang, Li-Sheng, Tu, Chi-Hsuan, Chang, Fan-Ren, Shei, Yen-Weay, Chang, Ching-Di, Tu, Kun-Yuan
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/796,479
• Time in Patent Office: 512 Days
• Field of Search: 342/357, 342/156, 342/424, 342/442, 701/215
• US Class Current: 342/357.31
• CPC Class Codes: G01S 19/55 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method
• CPC Class Codes: G01S 3/48 the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured

Abstract

The global positioning system (GPS) compass is consisted of three main units. These units are the pointer, the sensor, and the controller. The pointer unit is comprised of an iron frame, an aluminum bar, and two aluminum plates. The sensor unit is comprised of global positioning system (GPS) receivers and global positioning system (GPS) antennas. The controller unit includes a personal computer, a stepping motor, several data interface circuit boards, and some motor control circuit boards. The baseline of the pointer is an aluminum bar of about one meter long. The sensor unit can measure the baseline'"'"'s azimuth angle relative to the local coordinate. When command is received, the controller unit is capable of turning the aluminum bar to the desired direction by the aid of the stepping motor. There are two modes for operation available. One is the initial mode, the other is the normal mode. It takes about one or two minutes to complete the initial mode operation. In this mode, adjustment values needed in the algorithm for normal mode can be obtained upon rotating the aluminum bar at the baseline. The purpose of the initial mode is similar to an instrument calibration. In the normal mode, the global positioning system (GPS) compass can point itself to the desired direction in real time operation. In this invention, the combined use of attitude determination algorithm and stepping motor controlling technique, results in pointing deviation from accuracy to be less than 1 degree.

Claims

1. A global positioning system compass, comprising:

a pointer unit,

a sensor unit, and

a controller unit,

wherein the pointer unit includes a supporting frame, a metal bar supported by the supporting frame, and metal plates engaged with the metal bar and the sensor unit includes global positioning system antennas and global positioning system receivers.

2. The global positioning system compass defined by claim 1, wherein the controller unit includes a personal computer, at least one data interface circuit board, stepping motor and at least one controller circuit board, the stepping motor being supported by the supporting frame, a rotor axis of the motor being fixed with the metal bar, each of the metal plates being located on opposite ends of the metal bar, respectively,

each global positioning system antenna being respectively attached to one of the metal plates, the global positioning system antennas being connected to the global positioning system receivers and to a personal computer via data interface circuit boards, the personal computer including means for determining the attitude and for controlling the motor via motor controlling circuit boards.

3. The global positioning system compass defined by claim 1, wherein the supporting frame is made of an iron frame,

the metal bars and the metal plates are made of aluminum, and

the controller unit includes a personal computer, data interface circuit boards, stepping motor, and motor controlling circuit boards.

4. The global position system as defined by claim 1, wherein the sensor unit includes global positioning system antennas and global positioning system receivers.

5. A global positioning system compass, comprising:

a pointer unit,

a sensor unit, and

a controller unit,

wherein the pointer unit includes a supporting frame, a rigid bar, and metal plates.