Low-power satellite-based geopositioning system

• US 6,094,162 A
• Filed: 02/04/1999
• Issued: 07/25/2000
• Est. Priority Date: 11/20/1997
• Status: Expired due to Term

• Current Assignee: SkyBitz, Inc. (Ametek Incorporated)
• Original Assignee: SkyBitz, Inc. (Ametek Incorporated)
• Inventors: Sullivan, Mark
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US09/244,124
• Time in Patent Office: 537 Days
• Field of Search: 342/357.01, 342/457, 701/213, 375/207, 375/343
• US Class Current: 342/357.68
• CPC Class Codes: G01S 19/29 carrier including Doppler, related G01S19/246 takes precedence
• CPC Class Codes: G01S 19/30 code related G01S19/246 takes precedence
• CPC Class Codes: G01S 5/0246 involving frequency difference of arrival or Doppler measurements G01S5/02685 takes precedence
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial
• CPC Class Codes: H04B 7/18552 using a telephonic control signal and a second ranging satellite determining absolute distances from a plurality of spaced points of known location G01S5/14
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

A Low Earth Orbiting satellite system provides location and data communications services to mobile users equipped with a receiver/transmitter. The receiver/transmitter acts as a transponder that responds to a query transmitted over the satellite network. The response is sent after a precisely controlled time interval after the transponder receives the query so that the ground station can estimate the length of the propagation path from the satellite to the transponder. The transponder also transmits the response at a frequency that is proportional to the frequency of the received query so that the ground station can estimate the first and second derivatives of the length of the propagation path according to the measured Doppler shift. The ground station also estimates the satellite positioning using telemetry from the satellite obtained from the on-board GPS receiver. The position of the user terminal relative to the satellite position is then determined from the path length measurements. Given the satellite position and velocity, the measured path length and first and second derivatives determine the angle between the direction of satellite motion and the line of bearing to the user terminal. This angle defines a cone with the satellite at the origin. The user terminal position is somewhere on the circle defined by the cone and the estimated path length The intersection of this circle with the surface of the Earth yields two possible user positions, which ambiguity can be resolved by three techniques: (1) use of knowledge of which beam the signal was received in, (2) use of earlier position data; or (3) using nearby satellites to receive the signal. The user terminal uses a single frequency reference to provide timing for the receive and transmit frequency synthesizers and for the analog-to digital and digital-to-analog converters.

Claims

1. A transmitter for use in a geopositioning system, comprising:

a) a synchronization spreading code generator generating a synchronization code spreading signal;

b) a data spreading code generator generating a data code spreading signal;

c) a forward error corrector encoding user data for later error correction at a receive end;

d) a first modulator being coupled to the data code generator and the forward error corrector and modulating the encoded data on the data code spreading signal to form a data signal;

e) a first chip filter being coupled to first modulator and filtering the data signal,

f) a second chip filter being coupled to the synchronization code generator and filtering the synchronization code spreading signal;

g) a second modulator being coupled to the delay element;

h) a third modulator being coupled to the second chip filter,

i) a summer coupled to the second modulator and the third modulator and outputting a combined synchronization and data signal.

2. The transmitter according to claim 1, further comprising a delay element being coupled to the first chip filter and delaying one of the data or synchronization signals with respect to the other by one half chip.

3. The transmitter according to claim 1, wherein the synchronization and data spreading code generators produce repeated pairs of multilength chip sequences at a predetermined chip rate, and the data spreading sequence is modulated by a supercode at a predetermined data spreading sequence repetition rate.

4. The transmitter according to claim 3, wherein the synchronization spreading code generator produces a synchronization spreading sequence that is a multi-chip augmented maximal length pseudo random code, which is formed from a predetermined chip sequence that is augmented by adding a 0 to the predetermined sequence of consecutive 0'"'"'s.

5. The transmitter according to claim 3, wherein the data spreading code generator produces a data spreading sequence that is a multi-chip augmented maximal length pseudo random code, which is formed from a predetermined chip sequence that is augmented by adding a 0 to the predetermined sequence of consecutive 0'"'"'s.

6. The transmitter according to claim 3, wherein the forward error corrector produces a supercode sequence at a predetermined rate of code bits per second from a predetermined data stream, the forward error corrector includes two cascaded coders, a rate 1/3 convolutional coder and a orthogonal block coder, and an output of the forward error corrector is coupled to the first modulator mixed with an output from the data spreading code generator.

7. The transmitter according to claim 3, wherein the chip filters each accept digital data at a first data rate and produce interpolated and filtered baseband data at a higher data rate.

8. The transmitter according to claim 3, wherein a structure of data packets is different for the forward and reverse links, on the forward link, transmission is continuous and packets follow each other without interruption, whereas on the reverse link, individual units respond in a polled TDMA fashion.

9. The transmitter according to claim 1, wherein the third modulator is ninety degrees out of phase relative to the first quadrature modulator.