Low-cost satellite communication system

• US 8,494,443 B2
• Filed: 11/18/2004
• Issued: 07/23/2013
• Est. Priority Date: 03/21/1998
• Status: Active Grant

• Current Assignee: ORBCOMM SENS LLC (ORBCOMM Incorporated)
• Original Assignee: Comtech Mobile Datacom Corporation (Comtech Telecommunications Corporation)
• Inventors: Fleeter, Richard D., Hanson, John E., McDermott, Scott A., Zenick, Raymond G. Jr.
• Primary Examiner(s): Pan, Yuwen
• Assistant Examiner(s): Wang, Fanghwa
• Application Number:
  US10/992,173
• Publication Number:
  US 20050090199A1
• Time in Patent Office: 3,169 Days
• Field of Search: None
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/216 Code division or spread-spectrum multiple access [CDMA, SSMA]
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

A communication system is provided that allows the use of low-cost, low-power remote terminal units that communicate substantially asynchronously and independently to a base station. To minimize cost and complexity, the remote terminal units are configured similarly, including the use of substantially identical transmission schemes, such as a common Direct Sequence Spread Spectrum (DSSS) code. To minimize collisions among transmissions, the communication system is designed to use a high-gain antenna with a limited field of view, to limit the number of cotemporaneous, or overlapping transmissions that are received at the base station. To cover a wide area, the limited field of view is swept across the area of coverage. To overcome potential losses caused by collisions, the remote terminal units are configured to repeat transmissions; to minimize repeated collisions, the repeat interval and/or duration is randomized.

Claims

1. A satellite comprising:

a spacecraft control system that is configured to control the satellite;

a receiver that is configured to receive communications from a base station, on an uplink channel;

a transmitter that is configured to transmit communications to the base station on a downlink channel;

a controller that is configured to manage respective communications associated with the corresponding uplink and downlink channels; and

a satellite-based remote terminal unit operably coupled to the receiver, the transmitter, and the spacecraft control system, that is configured to;

monitor the communications from the base station for messages that are addressed to the satellite-based remote terminal unit,

communicate the communications that are addressed to the satellite-based remote terminal unit to the spacecraft control system, and

communicate messages from the spacecraft control system to the base station via the transmitter.

2. The satellite of claim 1, wherein:

the communications from the base station are modulated using a plurality of DSSS codes, and

the satellite-based remote terminal unit includes

a DSSS demodulator that is configured to demodulate a predetermined DSSS code of the plurality of DSSS codes, and

the communications that are addressed to the satellite-based remote terminal unit are modulated using the predetermined DSSS code.

3. The satellite of claim 1, wherein:

the communications from one or more remote terminal units are modulated using one or more DSSS codes, and

the satellite-based remote terminal unit includes

a DSSS modulator that is configured to modulate the messages using a predetermined DSSS code that differs from the one or more DSSS codes used by the remote terminal units.

4. The satellite s of claim 1, wherein:

the receiver is configured to provide the communications from the base station to the transmitter, and

the transmitter is further configured to

provide the subsequent retransmission of the communications from the base station to one or more remote terminal units.

5. The satellite of claim 1, wherein:

the receiver is further configured to;

receive the communications from a plurality of remote terminal units, and

provide the communications from the plurality of remote terminal units to the transmitter for transmission to the base station.