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Navigation
Volumn 42, Issue 1, 1995, Pages 165-185
Inertial Navigation Technology from 1970–1995
Author keywords

[No Author keywords available]
Indexed keywords

ACCELEROMETERS; COSTS; ELECTROMECHANICAL DEVICES; GYROSCOPES; PERFORMANCE; SENSORS; TECHNOLOGY;
EID: 0029275585     PISSN: 00281522     EISSN: 21614296     Source Type: Journal    
DOI: 10.1002/j.2161-4296.1995.tb02334.x     Document Type: Article
Times cited : (43)
References (54)
  • 1
    • 0026387042 scopus 로고
    • One notable exception is the cryogenically operated electrostatically supported gyroscope being developed by Stanford University for the Gravity Probe‐B mission. Development of the Gravity Probe‐B mission has spanned the entire period covered by this review. For more details about this system, see Everitt, C. F., The Stanford Gyroscope Experiment, Proceedings of the Conference on the Experimental Tests of Gravitation Theory, Jet Propulsion Laboratory Report TM‐33–499, Pasadena, CA, 1971; also available as NTIS N72‐13776. For a current reference, see, Calibration and Test of the World's Most Accurate Gyroscope, Proceedings of the Institute of Navigation National Technical Meeting, Phoenix, AZ, 2224
    • (1991) , pp. 217-227
    • Green, G.1    Kasdin, J.2    Ankeiser, M.3
  • 5
    • 84981665998 scopus 로고    scopus 로고
    • The thrust supplied by solid rocket motors used in these missiles is not easily regulated. The guidance and control system compensates for unintended fluctuations in missile velocity by controlling the vehicle attitude.
  • 10
    • 84981620953 scopus 로고
    • Evolution of the Peacekeeper Inertial Guidance Components and System Designs, AIAA Guidance Navigation and Control Conference, New Orleans, LA, Paper 91‐2762, pp., 1214
    • (1991) , pp. 1462-1470
    • Truncale, A.1
  • 11
    • 84981668760 scopus 로고
    • The Trident II (MK‐6) Guidance System, AIAA Guidance, Navigation and Control Conference, New Orleans, LA, Paper 91‐2761, pp., 1214
    • (1991) , pp. 1458-1461
    • Biren, M.A.1
  • 12
    • 84981668779 scopus 로고    scopus 로고
    • Minuteman III is still in service. The Poseidon Missile system was retired from the fleet in the early 1990s.
  • 13
    • 84981601394 scopus 로고
    • The PIPA (Pulsed Integrating Pendulous Accelerometer), MIT Instrumentation Laboratory Report E‐2334 (Apollo Guidance and Navigation)
    • (1968)
    • Bukow, G.1
  • 15
    • 84981673982 scopus 로고    scopus 로고
    • Advancements in Strapdown Navigation, NAECON 1974 Record, pp.
    • Roantree, J.P.1
  • 16
    • 84981616326 scopus 로고
    • Characteristic for a Medium Accuracy Inertial Navigation Set (INS), Technical Exhibit ENAC 77‐1, Revision 2, Change Notice 3, June 1982. Original release by USAF Aeronautical Systems Division
    • (1977)
  • 17
    • 84981659633 scopus 로고
    • Specification for USAF Standard Form, Fit and Function (F3) Medium Accuracy Inertial Navigation Unit, SNV84‐1, Rev. 3 Amendment 1,. Original release by USAF Aeronautical Systems Division, February 28, 1986.
    • (1987)
  • 18
    • 84981616306 scopus 로고
    • The Standard Inertial Navigation Set—A Decade of Progress, Proceedings of the 42nd Annual Meeting, The Institute of Navigation, Seattle, WA, 2426
    • (1986) , pp. 131-135
    • Lewi, J.1
  • 19
    • 84981663925 scopus 로고
    • LN‐40: The Fourth Generation Litton Inertial Navigation System, NACEON Record, pp.
    • (1975) , pp. 625-631
    • Lipman, J.S.1
  • 27
    • 84981571262 scopus 로고    scopus 로고
    • The discussion of RLGs that follows is admittedly of disproportionate length to the other topics in this summary.
  • 28
    • 84981639788 scopus 로고
    • An Overview of Optical Gyroscopes for Navigation, Paper No. 3 in, Integrated and Multi‐Function Navigation, AGARD CP‐525, Paris, France
    • (1992)
    • Mark, J.G.1    Tazartes, D.A.2
  • 29
    • 0016647191 scopus 로고    scopus 로고
    • The Honeywell Laser Inertial Navigation System (LINS), NAECON 1975 Conference Record, pp.
    • Savage, P.G.1
  • 36
    • 84981571265 scopus 로고
    • Projected Performance of Smaller Hemispherical Resonator Gyro, Proceedings of IEEE Position, Location and Navigation Symposium, PLANS 1986, Las Vegas, NV.
    • (1986)
    • Loper, E.J.1    Lynch, D.D.2    Stevenson, K.M.3
  • 38
    • 0020275952 scopus 로고
    • Vibrating Quartz Crystal Beam Accelerometer, Proceedings of the 28th International Instrumentation Symposium, Las Vegas, NV
    • (1982) , pp. 33-44
    • Albert, W.C.1
  • 39
    • 84981609390 scopus 로고
    • Low Cost Quartz Resonant Accelerometer for Aircraft Inertial Navigation, Proceedings of the IEEE International Conference on Solid State Sensors and Actuators, 2428
    • (1991)
    • Kourepenis, A.1    Petrovich, A.2    Weinberg, M.3
  • 45
  • 47
    • 84981575194 scopus 로고    scopus 로고
    • For example, relatively simple maneuvers such as banked turns can put 1 g or more of acceleration onto the horizontal axes of a strapped‐down INS. Compared with the time required for gyrocompassing, platform misalignment errors become rapidly observable as velocity errors when a sensor, such as GPS, provides independent velocity errors accurate to 0.1 ft/s.
  • 48
    • 84981669474 scopus 로고    scopus 로고
    • Advantages of Gimballed Inertial Navigation Systems, NAECON 1976 Record, pp.
    • Peterson, R.1
  • 51
    • 84981645774 scopus 로고
    • GPS/Inertial Integration
    • Parkinson, B., Enge, P., Axelrad, P., Spilker, J., AIAA, Washington, DC
    • (1995) GPS
    • Greenspan, R.L.1
  • 53
    • 84981609425 scopus 로고
    • Integrated NAV: The Second Edition I Never Wrote, to be presented at the 51st Annual Meeting of The Institute of Navigation, Colorado Springs, CO.
    • (1995)
    • Farrell, J.1

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.