Multi-antenna gas receiver for seismic survey vessels

• US 4,809,005 A
• Filed: 01/21/1988
• Issued: 02/28/1989
• Est. Priority Date: 03/01/1982
• Status: Expired due to Term

• Current Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Original Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Inventors: Counselman, III, Charles C.
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Sotomayor, John B.
• Application Number:
  US07/147,123
• Time in Patent Office: 404 Days
• Field of Search: 342/352, 342/357, 375/1
• US Class Current: 342/352
• CPC Class Codes: G01C 15/00 Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
• CPC Class Codes: G01S 19/04 providing carrier phase data
• CPC Class Codes: G01S 19/32 Multimode operation in a single same satellite system, e.g. GPS L1/L2
• CPC Class Codes: G01S 19/35 Constructional details or hardware or software details of the signal processing chain
• CPC Class Codes: G01V 1/3835 measuring position, e.g. by GPS or acoustically

Abstract

Method and apparatus are disclosed for accurately determining position from GPS satellites and received on a ship using observations of C/A code group delay, L1 band center frequency carrier phase, L1 band 5.115 MHz implicit carrier phase, and L2 band 5.115 MHz implicit carrier phase. A precise measurement of the range to each satellite is made based upon the L1 center frequency carrier phase. A correction for ionospheric effects is determined by simultaneous observation of the group delays of the wide bandwidth P code modulations in both the L1 and L2 bands. These group delays are determined by measuring the phases of carrier waves implicit in the spread-spectrum signals received in both bands. These carriers are reconstructed from both the L1 and L2 band signals from each satellite without using knowledge of the P code. The unknown biases in the L1 center frequency carrier phase range measurements are determined from simultaneous, pseudorange measurements, with time averaging. The instantaneous position of the antenna receiving these signals, and therefore the ship, may then be determined from the ranges so determined, with both the bias and the ionospheric effects having been eliminated. Additional antennas are positioned on the ship and a seismic streamer towed by the ship to reject false signals, compensate for blockage of signals by the ship'"'"'s structure, and determine the position of sensors in the streamer.

Claims

1. A method of determining ship towed sensor position information from code modulated, overlapping spread spectrum signals transmitted by a plurality of GPS satellites and modulated by satellite specific codes, comprising the steps of:

receiving a first composite of satellite signals related to ship position;

forming identical, synchronous, digital representations of the composite in a plurality of satellite tracking channels;

developing estimates in each tracking channel of group delay and phase delay, with respect to a common time base, of a satellite specific, code modulated component of the composite;

detecting a component in each channel by logical combination of the composite representation with a model of the component generated synchronously from the common time base in accordance with the estimates;

updating the estimates in accordance with the detected components to form time series of phase and group delay observations for each channel;

receiving a second composite of satellite signals related to sensor position;

forming a digital representations of the second composite;

developing an estimate of delay, with respect to the common time base, of a satellite specific, code modulated components of the second composite;

detecting said component by logical combination of the second composite representations with a model of the component generated synchronously from the common time base in accordance with the related estimate;

updating the estimate in accordance with the detected component to form time series of observations related to the second composite; and

processing the observations to determine sensor position.

2. The method of claim 1 further comprising:

updating the group delay estimate in response to changes of a predetermined magnitude in phase delay.

3. The method of claim 2 wherein the observation processing step further comprises:

deriving times series of instantaneous sensor position information by time averaging the observations over intervals long enough to include sensor position changes due to ship motion.

4. The method of claim 3 wherein the time averaging step further comprises:

taking differences between observations;

determining the average of the differences over a time period sufficiently long to include a plurality of independent observations from each time series; and

determining instantaneous sensor position information from the observations and the averaged differences therebetween.

5. The method of claim 4 wherein the sensor position information is determined from the difference between the phase observations and the averaged differences.

6. The method of claim 1 further comprising the steps of:

continuously monitoring an aspect of the detection to develop an indication of the validity thereof; and

inhibiting the updating of a particular estimate in response to the related validity indication.

7. The method of claim 6 wherein the estimate updating step further comprises:

changing the group delay observations by a predetermined magnitlude whenever a change in the group delay of the related component is detected.

8. The method of claim 7 further comprising:

adjusting the group delay estimate by a predetermined magnitude in response to changes of the same magnitude in the phase observations, uninhibited by the validity indication.

9. The method of claim 8 further comprising the steps of:

forming a time series of observations from a third composite of satellite signals related to another aspect of sensor position.