GPS Receiver Antijam Capability (dB)100908070605040302010100 kW10 kW1 kW100 W10 W1 W100 mWJAMMER ERP=10 mW010 20 30 40 50 60 70 80 90 100Range to Jammer (km)GPS Receiver Antijam Capability (dB)100908070605040302010ADVANCED RECEIVER WITH ADVANCED ANTENNAP(Y) CODE LOCK LOSS ADVANCED INTEGRATED RECEIVERP(Y) CODE LOCK LOSS CONVENTIONAL RECEIVERP(Y) CODE ACQUISITIONC/A CODE ACQUISITION100 kW10 kW1 kW100 W10 W1 W100 mWJAMMER ERP=10 mW010 20 30 40 50 60 70 80 90 100Range to Jammer (km)Figure 10. GPS jamming calculationsThe P(Y) code has more theoretical A/J protection than the C/Acode due to its ten times larger spread-spectrum bandwidth.Therefore, receivers have been developed that acquire the P(Y)code directly without having to acquire the C/A code first.However, because the P(Y) code is very long, a long time or manycorrelators are needed for a two-dimensional search over codetiming and Doppler frequency. It would be faster if satelliteephemerides and accurate code timing were available to performa “hot start.” For a GPS-aided weapon, accurate timing andsatellite position could be transferred from the aircraft to theweapon. This transfer normally requires a wide-band data bus;currently, few aircraft are so equipped.As new receiver technology with advanced algorithms andadaptive or nulling antenna technologies are incorporated into thesystem, increasing its A/J capability, A/J performance will improvesignificantly. Some possibilities are illustrated in Figure 11 (Ref.[14]). If A/J performance is increased significantly, then thejammer power must also be increased significantly. A largeFigure 11. Possible A/J capabilitiesjammer would present an inviting target to an antiradiation,homing missile. In the terminal area of flight against a target, thejammer located at the target will eventually jam the receiver andthe vehicle will have to depend on inertial-only guidance or theuse of a target sensor. Thus, it is important to ensure thataccurate guidance and navigation capability is provided to meetmilitary mission requirements against adversaries who are willingto invest in Electronic Countermeasures (ECM). This fact is truetoday and is expected to remain so in the foreseeable future.In summary, the following militarily-driven developments will beaccomplished in the near future to improve the A/J performanceof military systems:(1) Lower-cost but accurate inertial systems using newtechnologies such as micromechanical inertialinstruments and FOGs.(2) Highly integrated INS/GPS system architectures.(3) Higher-performance, lower-cost adaptive antennasusing digital beam forming and modern algorithms.INS/GPS Technology Trends for Military Systems12
Concluding RemarksRecent progress in INS/GPS technology has accelerated thepotential use of these integrated systems, while awareness has alsoincreased concerning vulnerabilities to jamming. In the nearfuture, improvements in accuracy in the broadcast GPS signalswill evolve to 1 m. Many uses will be found for this highaccuracy. In parallel, lower-cost inertial components will bedeveloped and they will also have improved accuracy. Highlyintegrated A/J architectures for INS/GPS systems will becomecommon, replacing avionics architectures based on functionalblack boxes where receivers and inertial systems are treated asstand-alone systems.Acknowledgments/Additional ReferencesThanks to Neil Barbour and John Elwell for assistance with thesection on Inertial Sensor Trends. A history of inertial navigationis given in Ref. [15] and the history of the GPS program is givenin Ref. [16].References[1] Barbour, N., J. Elwell, G. Schmidt, R. Setterlund, “InertialInstruments: Where to Now?,” <strong>Draper</strong> <strong>Laboratory</strong>,Cambridge, MA, May 1994. Presented at the 1st InternationalConference on Gyroscopic Technology, Elektropribor Institute,St. Petersburg, Russia, May 1994.[2] Barbour, N., K. Kumar, J. Elwell, “Emerging Low(er) CostInertial Sensors,” <strong>Draper</strong> <strong>Laboratory</strong> Report P-3399,Cambridge, MA, July 1994. Presented at the 22nd JointServices Data Exchange, Scottsdale, AZ, October 1994.[3] Snyder, S. et al., “INS/GPS Operational ConceptDemonstration (OCD) High Gear Program,” IEEE PLANSConference, April 1994, pp. 292-297.[4] National Research Council, The Global Positioning System - AShared National Asset, National Academy Press, Washington,D.C., 1995.[5] Butts, J. and C. Shank, “Navigation Message Correction Tables:A Proposal,” ION National Technical Meeting, January 1995,pp. 97-103.[6] Brottland, B. and C. Harris, “Navigation Message CorrectionTables: On Orbit Results,” ION 51st Annual Meeting, June1995, pp. 413-420.[7] Dargen, J. et al., “Exploitation of Differential GPS for GuidanceEnhancement (EDGE) High Gear Program,” NATO/AGARDMSP Meeting, Technologies for Precision Air Strike Operationsin Rapid Reaction and Localized Conflict Scenarios, Seville,Spain, October 1995.[8] Kelly, D. et al., “Navigation Performance Analysis for the EDGEProgram,” NATO/AGARD MSP Meeting, Technologies forPrecision Air Strike Operations in Rapid Reaction andLocalized Conflict Scenarios, Seville, Spain, October 1995.[9] Moeglein, M. et al., “Options for PPS Space Segment AccuracyEnhancement,” Navigation, Fall 1996, Vol. 43, No. 3, pp. 221-235.[10] Phillips, R. and G. Schmidt, “Relative and Differential GPS,” inNATO AGARD Lecture Series 207 on System Implications andInnovative Applications of Satellite Navigation, June 1996, pp.5.1-5.22.[11] Phillips, R. and G. Schmidt, “INS/GPS Integration,” in NATOAGARD Lecture Series 207 on System Implications andInnovative Applications of Satellite Navigation, June 1996, pp.9.1-9.18.[12] NAVSTAR-GPS Joint Program Office, NAVSTAR GPS UserEquipment, February 1991.[13] Mahmood, S. et al., “Analysis of Differential Global PositioningSystem (DGPS) Techniques and GPS Jamming on PrecisionGuided Munition (PGM) Performance,” NATO/AGARD MSPMeeting, Technologies for Precision Air Strike Operations inRapid Reaction and Localized Conflict Scenarios, Seville,Spain, October 1995.[14] Sklar, J., “GPS Capability Projections” in Defense Science Board1996 Summer Study Task Force on Tactics and Technology for21st Century Military Superiority, Vol. 3, October 1996, III.43-[15] <strong>Draper</strong>, C. S., “Origins of Inertial Navigation,” Journal ofGuidance and Control, Vol. 4, No. 5, 1981, pp. 449-463.[16] Parkinson, B., “Origins, Evolution, and Future of SatelliteNavigation,” Journal of Guidance, Control, and Dynamics, Vol.20, No. 1, 1997, pp. 11-25.INS/GPS Technology Trends for Military Systems13
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Letter from thePresident and CEO,Vi
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Information TechnologyMilton AdamsE
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BiographyMilton Adams has been at D
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AcknowledgmentR.L. Greenspan, J.A.
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Systems IntegrationRich MartoranaPe
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The 1997 Charles StarkDraper PrizeT
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The 1997 Charles StarkDraper Prize1
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“Draper encourages its personnel
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Gimballed Vibrating GyroscopeHaving
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Optical Source Isolator withPolariz
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Hunting Suppressor forPolyphase Ele
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1997 Published PapersThe following
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monitoring of space structures and
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McConley, M. W.; Dahleh, M. A.; Fer
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unaffordable, or even misguided. Bu
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