Positioning system for a vehicle

• US 4,731,613 A
• Filed: 12/04/1985
• Issued: 03/15/1988
• Est. Priority Date: 12/07/1984
• Status: Expired due to Fees

• Current Assignee: Nissan Motor Co., Ltd.
• Original Assignee: Nissan Motor Co., Ltd.
• Inventors: Endo, Hiroshi, Hirano, Motoki, Fukuhara, Hiroshige
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Issing, Gregory C.
• Application Number:
  US06/804,511
• Time in Patent Office: 832 Days
• Field of Search: 343/356, 343/357, 343/451, 343/457, 343/461, 364/450, 364/451
• US Class Current: 342/357.31
• CPC Class Codes: G01C 21/28 with correlation of data from several navigational instruments
• CPC Class Codes: G01S 19/42 Determining position

Abstract

An improved positioning system for a vehicle is shown. In the system, when radio wave can be received from only one satellite, the current position of the vehicle is computed based on a pair of navigational data, which are brought by radio wave received at the current time and by radio wave received at an earlier time.

Claims

1. A system for measuring the position of an object comprising:

receiving means for receiving navigational data radiated from a plurality of satellites and calculating position data and propagating delay time data based on the navigational data received from the plurality of satellites;

computing means, coupled to said receiving means, for calculating the position of the object when said receiving means receives navigational data from at least three satellites, based on the position data and the propagating delay time data calculated by the receiving means;

vector means for detecting the velocity and the angular velocity of the object and calculating a shifted vector amount caused by the displacement of the object during a predetermined time interval based on the detected velocity and the detected angular velocity of the object; and

compound computing means, coupled to said receiving means and said vector means, for calculating the position of the object when said receiving means receives data from at least one satellite but less than three satellites, based on the position data and the propagating delay time data calculated by the receiving means and the shifted vector amount calculated by the vector means.

2. A measuring system as claimed in claim 1 wherein said compound computing means calculates a first circle on which the object is located by intersecting the earth'"'"'s sphere and a sphere around one of the satellites on the basis of the propagating delay time data received from the receiving means, and calculating a displaced circle by displacing the first circle based on the shifted vector amount received from the vector means, said compound computing means further calculating a second circle on which the object is located on the basis of the propagating delay time data received from the receiving means after the predetermined time interval, by intersecting the earth'"'"'s sphere and a sphere around one of the satellites, and calculating the position of the object by intersecting the displaced circle and the second circle.

3. A measuring system as claimed in claim 1, wherein said computing means comprises GPS computing means which determines the position of the object on the basis of the navigational datal received from at least three satellites.

4. A measuring system as claimed in claim 1 further comprising guidance means, coupled to the computing means, the vector means and the compound computing means, for displaying the position of the object, said guidance means displaying the position of the object received from said computing means when said receiving means receives navigational data from at least three satellites, the position of the object received from the compound computing means when said receiving means receives navigational data from at least one and less than three satellites, and the position of the object based on the shifted vector amount received from said vector means when said receiving means receives no navigational data.

5. A measuring system as claimed in claim 4, wherein the position of the object is calculated according to the spherical coordinates of the earth with a radial variable constantly fixed to the earth'"'"'s radius.

6. A measuring system as claimed in claim 5, wherein the constant radial variable is corrected using geoid.

7. A measuring system as claimed in claim 6, wherein said measuring system further comprises an altimeter measuring the altitude of the object and further correctng the constant radial variable.

8. A measuring system as claimed in claim 1, wherein said vector means comprises an optical fiber gyro for detecting the angular velocity of the object and a sensor for sensing the velocity of the object.