Stem orientation measurement apparatus

• US 4,644,358 A
• Filed: 06/23/1983
• Issued: 02/17/1987
• Est. Priority Date: 11/13/1982
• Status: Expired due to Term

• Current Assignee: Nihon Musen Kabushiki Kaisha
• Original Assignee: Nihon Musen Kabushiki Kaisha
• Inventors: Sekine, Chogo
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Issing, Gregory C.
• Application Number:
  US06/507,017
• Time in Patent Office: 1,335 Days
• Field of Search: 348/355-357, 348/405, 348/418, 348/428, 348/433, 348/434, 348/449, 348/458, 343/352
• US Class Current: 342/356
• CPC Class Codes: G01S 19/53 Determining attitude
• CPC Class Codes: G01S 3/52 using a receiving antenna moving, or appearing to move, in a cyclic path to produce a Doppler variation of frequency of the received signal

Abstract

An apparatus to confirm an orientation of the stem of ship by making use of a satellite included in the Global Positioning System. Radio wave signals from the satellite are received by a directional or omnidirectional antenna and the phase difference between a rotating period of said antenna and either the period of distance fluctuation, Doppler fluctuation, phase fluctuation or amplitude fluctuation is detected to obtain an orientation of the satellite which is used to obtain an accurate orientation of the stem relative to a reference direction such as due North.

Claims

1. A stem orientation measurement apparatus, comprising:

an antenna receiving GPS radio waves,

means for effectively rotating said antenna,

a GPS receiver for providing information about a location of a ship and an orientation of a GPS satellite,

means for determining the fluctuation of received radio waves from said GPS satellite based on a PN code of said GPS satellite transmitted from said GPS receiver, the timing of said PN code and GPS signals received by said antenna,

means for detecting said orientation of said GPS satellite relative to the orientation of the stem by detecting a phase difference between a period of fluctuation of said received wave and a period of rotation of said antenna,

means for determining said orientation of the stem relative to a reference direction from said orientation of said GPS satellite, and

an indicator for indicating said orientation of the stem.

2. An apparatus as set forth in claim 1, wherein said antenna comprises a plurality of omnidirectional antennas which are disposed on a circle and are sequentially activated for a given period.

3. An apparatus as set forth in claim 1, wherein said antenna comprises at least one directional antenna which effectively rotates.

4. An apparatus as set forth in claim 2, wherein said antenna comprises at least four (4) dipole antennas.

5. An apparatus as set forth in claim 1, wherein said means for determining the fluctuation of received radio waves from said GPS satellite determines the distance from said GPS satellite to said antenna.

6. An apparatus as set forth in claim 1, wherein said means for determining the fluctuation of received radio waves from said GPS satellite determines the Doppler fluctuation of said received radio waves from said GPS satellite.

7. An apparatus as set forth in claim 1, wherein said means for determining the fluctuation of received radio waves from said GPS satellite determines phase fluctuation of said received radio waves from said GPS satellite.

8. An apparatus as set forth in claim 1, wherein said means for determining the fluctuation of received radio waves from said GPS satellite determines the amplitude fluctuation of said received radio waves from said GPS satellite.