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• W2094896067 abstract "No AccessHistory of Key TechnologiesBlazing Gyros: The Evolution of Strapdown Inertial Navigation Technology for AircraftPaul G. SavagePaul G. SavageStrapdown Associates, Inc., Maple Plain, Minnesota 55359Search for more papers by this authorPublished Online:19 Mar 2013https://doi.org/10.2514/1.60211SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] MacKenzie D., Inventing Accuracy, MIT Press, Cambridge, MA, 1993, pp. 71–92, Chap. 2. Google Scholar[2] Minor J. W., “Low-Cost Strapdown-Down Inertial Systems,” AIAA/ION Guidance and Control Conference, Aug. 1965. Google Scholar[3] Eberlein A. J. and Savage P. G., “Strapdown Cost Trend Study and Forecast,” NASA Ames Research Center CR-137585, 1 Jan. 1975. Google Scholar[4] Shaw J. 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J., “Ring Laser Device Performs Rate Gyro Angular Rate Sensor Functions,” Aviation Week and Space Technology, 11 Feb. 1963, pp. 98–103. AWSTAV 0005-2175 Google Scholar[11] Savage P. G., “Strapdown Sensors,” Strapdown Inertial Systems: Theory And Applications, NATO AGARD-LS-95, June 1978, Sec. 2. Google Scholar[12] Savage P. G., “Advances in Strapdown Sensors,” Advances in Strapdown Inertial Systems, NATO, AGARD-LS-133, 14–15 May 1984. Google Scholar[13] Warzynski R. R. and Ringo R. L., “The Evolution of ESG Technology,” 15th Meeting of the Guidance and Control Panel of AGARD, Florence, Italy, Oct. 1972, pp. 13-1–13-8. Google Scholar[14] Lawrence A., Modern Inertial Technology, Springer–Verlag, New York, 1993, pp. 93–147. CrossrefGoogle Scholar[15] Merhav S., Aerospace Sensor Systems and Applications, Springer–Verlag, New York, 1996, pp. 186–271. CrossrefGoogle Scholar[16] Sinkiewicz J. S., Feldman J. and Lory C. 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JOSAAH 0030-3941 Google Scholar[27] United Aircraft Corporate Systems Center, “A Study of Critical Computational Problems Associated with Strapdown Inertial Navigation Systems,” NASA Rept. CR-968, April 1968. Google Scholar[28] Savage P.G., “A New Second-Order Solution for Strapped-Down Attitude Computation,” AIAA Joint Automatic Control Conference, Aug. 1966. Google Scholar[29] Bortz J. E., “A New Concept in Strapdown Inertial Navigation,” Ph.D. Dissertation, Massachusetts Inst. of Technology, Cambridge, MA, June 1969. Google Scholar[30] Jordan J. W., “An Accurate Strapdown Direction Cosine Algorithm,” NASA TN-D-5384, Sept. 1969. Google Scholar[31] Savage P. G., “Strapdown System Algorithms,” Advances in Strapdown Inertial Systems, NATO, AGARD-LS-133, May 1984, Sec. 3. Google Scholar[32] Savage P. 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G., “Coning Algorithm Design by Explicit Frequency Shaping,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 4, 2010, pp. 1123–1132. doi:https://doi.org/10.2514/1.47337 JGCDDT 0162-3192 LinkGoogle Scholar[41] Savage P. G., “Explicit Frequency Shaped Coning Algorithms for Pseudoconing Environments,” Journal of Guidance, Control, and Dynamics, Vol. 34, No. 3, 2011, pp. 774–782. doi:https://doi.org/10.2514/1.51600 JGCDDT 0162-3192 LinkGoogle Scholar[42] Podgorski T. J. and Thymian D. M., “Design and Development of the AA1300Ad02 Laser Gyro,” NASA Rept. CR-132261, pp. 10–11. Google Scholar[43] Savage P. G., “The Honeywell Laser Inertial Navigation System (LINS),” IEEE National Aerospace & Electronics Conference (NAECON), June 1975. Google Scholar[44] Savage P. G. and Ignagni M. B., “Honeywell Laser Inertial Navigation System (LINS) Test Results,” IEEE Ninth Joint Services Data Exchange Group for Inertial Systems, Nov. 1975. Google Scholar[45] Savage P. G., “Laser Gyros in Strapdown Inertial Navigation Systems,” IEEE Position Location and Navigation Symposium, Nov. 1976. Google Scholar[46] Duncan R. R., “MICRON–A Strapdown Inertial Navigator Using Miniature Electrostatic Gyros,” SAE Aerospace Control and Guidance Systems Committee, May 1974. Google Scholar[47] Fenner P. J., “Requirements, Applications, and Results of Strapdown Inertial Technology to Commercial Airplanes,” Advances in Strapdown Inertial Systems, NATO AGARD-LS-133, May 1984. Google Scholar[48] “RV ‘Flies’ Through On-The-Ground Tests”, Onan On The Road…, Vol. 3, Onan News, 1975, pp. 4–5. Google Scholar[49] Payne D. P., Shoaf R. B. and Koesters H. P., “Development Test of the Honeywell Laser Inertial Navigation System (LINS),” Central Inertial Guidance Test Facility, 6585th Test Group, Final Rept. ADTC-TR-75-74, Holloman AFB, Nov. 1975. Google Scholar[50] Bachman K. and Skoyles R., “Advanced Development Model Ring Laser Gyro Navigator, A-7E Aircraft Flight Test Results,” U.S. Naval Air Development Center Rept. NADC-80058-40, 15 Aug. 1980. Google Scholar[51] Bachman K. L., “Ring Laser Gyro Navigator (RLGN) Flight Test Results,” Navigation, Vol. 28 No. 3, 1981, pp. 214–223. NVGNAL 0028-1530 CrossrefGoogle Scholar[52] Savage P. G., “Calibration Procedures for Laser Gyro Strapdown Inertial Navigation Systems,” 9th Annual Electro-Optics/Laser Conference and Exhibition, Oct. 1977. Google Scholar[53] Miller J. M. and et al., “Micro Navigator (MICRON) Phase 2A Volume I – Technical Report,” AFAL-TR-75-210, Feb. 1976. Google Scholar[54] Volk C. H., Gillespie S. C., Mark J. G. and Tazartes D. A., “Multioscillator Ring Laser Gyroscopes and Their Applications,” Optical Gyros and Their Applications, AGARDograph Rept. 339, June 1999. Google Scholar[55] Savage P. G., Introduction to Strapdown Inertial Navigation Systems, 12th ed., Strapdown Assoc., Maple Plain, MN, 10 Jan. 2010, pp. 327A–327D. Google Scholar[56] Sebring D. L., Perdzock J. M. and Young J. T., “Application of Multifunction Strapdown Inertial System,” Advances in Strapdown Inertial Systems, NATO AGARD Lecture Series No. 133, May 1984, Sec. 8. Google Scholar Next article" @default.
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