Wireless communication system

• US 5,646,761 A
• Filed: 09/05/1995
• Issued: 07/08/1997
• Est. Priority Date: 09/24/1993
• Status: Expired due to Term

• Current Assignee: Jolt Ltd (MRV Communications Incorporated)
• Original Assignee: Jolt Ltd (MRV Communications Incorporated)
• Inventors: Medved, David, Davidovich, Leonid, Bar Lev, Hillel
• Primary Examiner(s): Williams, Hezron E.
• Assistant Examiner(s): Moller, Richard A.
• Application Number:
  US08/522,526
• Time in Patent Office: 672 Days
• Field of Search: 359/152, 359/154, 359/155, 359/172
• US Class Current: 398/123
• CPC Class Codes: H04B 10/1143 Bidirectional transmission

Abstract

A wireless communication system, having first and second communication units located, in operation, in spaced-apart relationship to each other, each unit including a transmitter and a receiver, the first unit including a transmitter for transmitting information to the receiver of the second unit, and a receiver for receiving information from the transmitter of the second unit, the first unit including a scanner for scanning the unit along at least one axis with respect to the second unit. The first unit further includes a control for terminating the scanning of the first unit when the receiver of the first unit is precisely aligned with the transmitter of the second unit.

Claims

1. A wireless data communication system for communicating between an airplane and a ground loading terminal, comprising:

a. a ground communication unit coupled to a ground terminal and mounted on a loading gateway adapted to approach and engage a parked airplane to enable loading and unloading of the airplane, said ground communication unit including a ground communication infrared transmitter transmitting a fan shaped infrared beam with a pattern which is narrower in the horizontal direction and wider in the vertical direction and comprising a plurality of infrared devices oriented to transmit said fan shaped infrared beam, an elevation scanning means comprising switching means for selectively energizing said plurality of infrared devices, azimuth scanning means driven by a stepping motor for scanning in a substantially horizontal direction with respect to the ground, a ground communication receiver comprising an infrared detector for detecting an infrared beam and having a field of view which is narrower in the horizontal direction and wider in the vertical direction, and a controller for controlling the operation of said ground communication unit elevation and azimuth scanning means;

b. an airplane communication unit including an airplane communication infrared transmitter transmitting a fan shaped infrared beam with a pattern which is a narrower in the horizontal direction and wider in the vertical direction and comprising a plurality of infrared devices oriented to transmit said fan shaped infrared beam, an elevation scanning means comprising switching means for a selectively energizing said plurality of infrared devices, azimuth scanning means driven by a stepping motor for scanning in a substantially horizontal direction with respect to the ground, an airplane communication receiver comprising an infrared detector for detecting an infrared beam and having a field of view which is narrower in the horizontal direction and wider in the vertical direction, and a control means for controlling the operation of the airplane communication unit elevation and azimuth scanning means;

c. wherein the infrared transmitter of the airplane communication unit and the infrared transmitter of the ground communication unit are fixed a predetermined distance from the receiver of that same unit, which distance is substantially the same for both the airplane communication unit and the ground communication unit, such that when the receiver of the airplane communication unit is aligned with the transmitter of the ground communication unit, the transmitter of the airplane communication unit is also aligned with the receiver of the ground communication unit;

d. said controller of the ground communication unit terminates scanning of said ground communication unit elevation and azimuth scanning means when the receiver of said ground communication unit receives the infrared beam transmitted from the transmitter of said airplane communication unit;

e. said control means of the airplane communication unit terminates operation of its elevation and azimuth scanning means when its receiver becomes aligned with the transmitter of the ground communication unit, and maintains the operation terminated even when its receiver becomes misaligned with the transmitter of the ground communication unit by the operation of the scanning means of the ground communication unit, but restarts operation of its elevation and azimuth scanning means when its receiver fails to become realigned with the transmitter of the ground communication unit after a predetermined time interval.

2. The system according to claim 1, wherein each azimuth scanning means stepping motor oscillates its respective unit horizontally about a vertical axis for a sector of a circle.

3. The system according to claim 1, wherein the stepping motor of the azimuth scanning means of the airplane communication unit effects about thirty scanning cycles per minute.

4. The system according to claim 1, wherein the stepping motor of the azimuth scanning means of the ground communication unit effects about three hundred scanning cycles per minute.

5. The system according to claim 1, wherein each of said infrared transmitters includes three infrared devices, and each said switching means selectively energizes the infrared devices a plurality of times for each step of the stepping motor.

6. The system according to claim 1, wherein the azimuth scanning means of said airplane communication unit operates at a slower speed than the azimuth scanning means of said ground communication unit.

7. The system according to claim 1, wherein said control means of the airplane communication unit, before restarting operation of its scanning means, first displaces the airplane communication unit a single step in a first direction, and then two steps in a second direction opposite to said first direction.

8. The system according to claim 1, wherein one of said units includes a drive means for effecting a controlled reciprocating motion of that unit.

9. The system as claimed in claim 8, wherein said drive means includes a mechanical arrangement imparting combined linear and angular motions to said one unit.

10. The system according to claim 2, wherein the azimuth scanning means of said airplane communication unit operates at a slower speed than the azimuth scanning means of said ground communication unit.

11. The system according to claim 10, wherein the stepping motor of the azimuth scanning means of the airplane communication unit effects about thirty scanning cycles per minute.

12. The system according to claim 11, wherein the stepping motor of the azimuth scanning means of the ground communication unit effects about three hundred scanning cycles per minute.

13. The system according to claim 12, wherein each of said infrared transmitters includes three infrared devices, and each said switching means selectively energizes the infrared devices a plurality of times for each step of the stepping motor.

14. The system according to claim 13, wherein said control means of the airplane communication unit, before restarting operation of its scanning means, first displaces the airplane communication unit a single step in a first direction, and then two steps in a second direction opposite to said first direction.

15. The system according to claim 14, wherein one of said units includes a drive means for effecting a controlled reciprocating motion of that unit.

16. The system according to claim 15, wherein said drive means includes a mechanical arrangement imparting combined linear and angular motions to said one unit.