Switching control for multiple fiber-guided missile systems

• US 5,443,227 A
• Filed: 10/15/1993
• Issued: 08/22/1995
• Est. Priority Date: 10/15/1993
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Hsu, Hui-Pin
• Primary Examiner(s): Lobo, Ian J.
• Application Number:
  US08/136,190
• Time in Patent Office: 676 Days
• Field of Search: 244/3.12, 359/123, 359/135, 359/137, 359/139, 359/165, 370/50
• US Class Current: 244/3.12
• CPC Class Codes: H04J 14/0298 with sub-carrier multiplexing [SCM]

Abstract

A fast and reliable switch (50) for multi-channel, bi-directional fiber optics data link (FODL) systems. The FODL channel switching is accomplished through a software command on the subcarrier frequency (SCF) code without using any moving components or wavelength sensitive optical devices. A fiber star coupler (92) and in-line erbium doped fiber amplifiers (94A-94Q) transform the FODL system into an electrically switchable, fiber star network with low optical power loss penalty. The switch can be used in multiple fiber optics guided missile launch systems and fiber optics based surveillance systems with multiple outposts. The switching scheme allows the launcher/controller (60) to perform a time-sharing control on multiple missiles (or outposts) (80-80P) by switching the SCF code sent to the programmable SCF generator of the OE unit in the controller (launcher). The scheme can also easily be extended to operate in a multiple control station mode that uses multiple control station at the launcher/controller (60) to control multiple missiles or outposts (80A-80P).

Claims

1. A multi-channel, bi-directional fiber optic data link (FODL) system, comprising Q uplink fiber optic channels, P downlink fiber optic channels, a fiber optic star coupler for coupling said Q uplink fiber optic channels and said P downlink channels, P remote platform opto-electronic (OE) units respectively connected to said P downlink fiber optic channels, Q control station OE units respectively connected to said Q uplink channels, and a controller for providing remote platform commands addressed to said remote platform OE units for communication over said uplink channels in a time division multiplexed (TDM) scheme, said commands comprising a subcarrier frequency (SCF) code specifying a subcarrier frequency to be utilized by a particular remote platform OE unit to which said command is addressed, said remote platform OE units comprising programmable means responsive to said commands for generating an upconversion subcarrier signal at a subcarrier frequency determined by said SCF code to up-convert remote platform data for downlink transmission to said controller.

2. The FODL system of claim 1 wherein said uplink channels have an uplink data rate, said downlink channels have a downlink data rate, and wherein said downlink data rate is substantially higher than said uplink data rate.

3. The FODL system of claim 1 wherein each of said Q control station OE units respectively comprises a downlink receiver responsive to downlink signals received from said star coupler for providing receiver signals, means for generating a local oscillator (LO) signal, said means responsive to a corresponding SCF code to select said LO signal in dependence on said SCF code from said controller, and mixing means for mixing said receiver signals with said LO signal to down-convert said receiver signals.

4. The FODL system of claim 3 wherein each said control station OE units has associated therewith a different SCF code.

5. The FODL system of claim 3 wherein said means for generating said LO signal comprises a programmable SCF generator comprising an oscillator driving a phase locked loop comprising a phase comparator, a divide-by-N circuit whose value of N is set by said SCF code, and a voltage controlled oscillator whose output is said LO signal.

6. The FODL system of claim 1 wherein said star coupler comprises signal amplification means for optically amplifying said uplink and downlink signals.

7. The FODL system of claim 6 wherein said amplification means comprises a diode laser pump which injects its power through an auxiliary input port of said fiber star coupler, and a plurality of optical fiber amplifiers sharing said laser pump.

8. The FODL system of claim 1 wherein each of said remote platform OE units comprises an uplink receiver for recovering said time division multiplexed commands and SCF codes, and means for providing said recovered SCF codes to said means for generating said upconversion subcarrier signal.

9. The FODL system of claim 8 wherein said means for generating said upconversion subcarrier signal comprises a programmable SCF generator comprising an oscillator driving a phase locked loop comprising a phase comparator, a divide-by-N circuit whose value of N is set by said SCF code, and a voltage controlled oscillator whose output is said upconversion subcarrier signal.

10. The FODL system of claim 1 wherein said remote platform unit further comprises means for mixing said upconversion subcarrier signal with said platform data to provide a subcarrier modulated signal.

11. The FODL system of claim 10 wherein said remote platform unit further comprises a downlink transmitter responsive to said subcarrier modulated signal.

12. The FODL system of claim 1 further comprising a data multiplexer for combining signals from a plurality of platform data sources to form a serial digital data stream.

13. The FODL system of claim 1 wherein said platform data comprises global position system data signals.

14. The FODL system of claim 1 wherein said platform data comprises digitized video data.

15. The FODL system of claim 1 wherein said platform data comprises telemetry data.

16. A missile system comprising:

P fiber guided missiles;

a missile launcher controller for controlling said missiles; and

a multi-channel, bi-directional fiber optic data link (FODL) system, comprising;

Q uplink fiber optic channels;

P downlink fiber optic channels;

a fiber optic star coupler for coupling said Q uplink fiber optic channels and said P downlink channels;

P missile opto-electronic (OE) units respectively connected to said P downlink fiber optic channels;

Q launcher control station OE units respectively connected to said Q uplink channels; and

a controller for providing remote platform commands addressed to said missile opto-electronic (OE) units for communication over said uplink channels in a time division multiplexed scheme, said commands comprising a subcarrier frequency (SCF) code specifying a subcarrier frequency to be utilized by a particular missile OE unit to which said command is addressed, said missile OE units comprising programmable means responsive to said commands for generating an upconversion subcarrier signal at a subcarrier frequency determined by said SCF code to upconvert remote platform data for downlink transmission to said launcher controller.

17. The missile system of claim 16 wherein said uplink channels have an uplink data rate, said downlink channels have a downlink data rate, and wherein said downlink data rate is substantially higher than said uplink data rate.

18. The missile system of claim 16 said Q control station OE units respectively comprises a downlink receiver responsive to downlink signals received from said star coupler for providing receiver signals, means for generating a local oscillator (LO) signal, said means responsive to a corresponding SCF code to select said LO signal in dependence on said SCF code, and mixing means for mixing said receiver signals with said LO signals to down-convert said receiver signals.

19. The missile system of claim 18 wherein each said control station OE units has associated therewith a different SCF code.

20. The missile system of claim 18 wherein said means for generating said LO signal comprises a programmable SCF generator comprising an oscillator driving a phase locked loop comprising a phase comparator, a divide-by-N circuit whose value of N is set by said SCF code, and a voltage controlled oscillator whose output is said LO signal.

21. The missile system of claim 16 wherein said star coupler comprises signal distribution means for distributing optical signals from any of P channels among all Q channels, and signal amplification means for optically amplifying optical signals carried on said uplink and downlink optical channels.

22. The missile system of claim 21 wherein said amplification means comprises a diode laser pump which injects its power through an auxiliary input port of said coupler, and a plurality of optical fiber amplifiers sharing said laser pump.

23. The missile system of claim 16 wherein said missile OE units each comprise an uplink receiver for recovering said commands, and means for providing said recovered SCF commands to said means for generating said upconversion subcarrier signal.

24. The missile system of claim 23 wherein said means for generating said upconversion subcarrier signal comprises a programmable SCF generator comprising an oscillator driving a phase locked loop comprising a phase comparator, a divide-by-N circuit whose value of N is set by said SCF code, and a voltage controlled oscillator whose output is said upconversion subcarrier signal.

25. The missile system of claim 16 wherein said remote platform unit further comprises means for mixing said upconversion subcarrier signal with said platform data to provide a subcarrier modulated signal.

26. The missile system of claim 24 wherein said remote platform unit further comprises a downlink optical transmitter responsive to said subcarrier modulated signal.

27. The missile system of claim 16 further comprising a data multiplexer for combining signals from a plurality of platform data sources to form a serial digital data stream.

28. The missile system of claim 16 wherein said platform data comprises global position system data signals.

29. The missile system of claim 16 wherein said platform data comprises digitized video data.

30. The missile system of claim 16 wherein said platform data comprises telemetry data.