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Volumn 134, Issue , 2009, Pages 1157-1178

The hemispherical resonator gyro: From wineglass to the planets

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN AND OPERATIONS; HEMISPHERICAL RESONATOR GYROS; LOW NOISE; MISSION SUCCESS; PLANETARY EXPLORATION; SMALL SIZE; SPACE MISSIONS;

EID: 80053425227     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (301)

References (19)
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    • (1835) J. Ec. Polytech. , vol.15 , pp. 142-154
    • Coriolis, G.G.1
  • 2
    • 0001576469 scopus 로고
    • On the beats in the vibrations of a revolving cylinder or bell
    • Nov. 24
    • Bryan, G. H., On the Beats in the Vibrations of a Revolving Cylinder or Bell, Cambridge Phil. Soc., vol. VII, pt. III, p. 101, Nov. 24, 1890
    • (1890) Cambridge Phil. Soc. , vol.7 , Issue.PART. 3 , pp. 101
    • Bryan, G.H.1
  • 3
  • 4
    • 80053434176 scopus 로고    scopus 로고
    • Delco Systems-AC Electronics 1948-2004 History
    • Voros, Art. Gyro and Accelerometer History, Delco Systems-AC Electronics 1948-2004 History, 2008, page 4
    • (2008) Gyro and Accelerometer History , pp. 4
    • Voros, A.1
  • 6
    • 80053412267 scopus 로고
    • Delco Electronics Division report R77-64 August, NAVY contract no N00123-76-C-1445 (for NWC, China Lake, CA)
    • Final Technical Report: Sonic Gyro Fabrication and Testing, Delco Electronics Division, report R77-64, August 1977. NAVY contract no. N00123-76-C-1445 (for NWC, China Lake, CA)
    • (1977) Final Technical Report: Sonic Gyro Fabrication and Testing
  • 12
    • 80053394761 scopus 로고
    • Ultra-reliable fault-tolerant inertial reference unit for spacecraft
    • Keystone, Colorado , paper AAS 94-022
    • Sinaki, George, Ultra-reliable fault-tolerant inertial reference unit for spacecraft, 17th Annual AAS Guidance and Control Conference, Keystone, Colorado (1994).paper AAS 94-022, page 4
    • (1994) 17th Annual AAS Guidance and Control Conference , pp. 4
    • Sinaki, G.1
  • 13
    • 84255184242 scopus 로고    scopus 로고
    • Hemispherical resonator gyro noise reduction for precision spacecraft pointing
    • February 7-11, Breckenridge, CO. paper AAS 96-006
    • Matthews, Anthony and Bauer, David A., Hemispherical Resonator Gyro Noise Reduction for Precision Spacecraft Pointing, 19th Annual AAS Guidance And Control Conference, February 7-11, 1996, Breckenridge, CO. paper AAS 96-006, page 4
    • (1996) 19th Annual AAS Guidance and Control Conference , pp. 4
    • Matthews, A.1    Bauer, D.A.2
  • 14
    • 80053409948 scopus 로고    scopus 로고
    • Dual use HRG for space and subterranean applications
    • Coco Beach, FL, 29 April
    • th Space Congress, Coco Beach, FL, 29 April 1997. Pages 10-11
    • (1997) th Space Congress , pp. 10-11
    • Matthews, A.1
  • 15
    • 80053421196 scopus 로고    scopus 로고
    • Northrop grumman's scalable space inertial reference unit: Innovations reduced to practice
    • Colorado, February.,AAS - 02-039
    • Ciolino, Richard, et. al., Northrop Grumman's Scalable Space Inertial Reference Unit: Innovations Reduced to Practice, 25th Annual Guidance and Control Conference, Breckenridge, Colorado, February 2002.,AAS -02-039
    • (2002) 25th Annual Guidance and Control Conference, Breckenridge
    • Ciolino, R.1
  • 17
    • 80053434677 scopus 로고    scopus 로고
    • Development of the HRG based scalable space inertial reference unit for long- life moderate and precision pointing spacecraft
    • January 31 - February 4, Breckenridge, CO. AAS 01-034
    • Johnson, Gregory M., et. al., Development of the HRG Based Scalable Space Inertial Reference Unit for Long- Life Moderate and Precision Pointing Spacecraft, 24th Annual AAS Guidance And Control Conference, January 31 - February 4, 2001, Breckenridge, CO. AAS 01-034, pages 4-5.
    • (2001) 24th Annual AAS Guidance and Control Conference , pp. 4-5
    • Johnson, G.M.1
  • 18
    • 80053405843 scopus 로고    scopus 로고
    • Flight experience of the space inertial reference unit utilizing the solid state HRG
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    • Londerville, G., et. al., In-Flight Experience of the Space Inertial Reference Unit Utilizing the Solid State HRG, Proceedings Third International Conference on Spacecraft Guidance, Navigation and Control Systems, ESTEC, Noordwijk, Netherlands, 26-29 November 1996, ESA SP-381 (Published February 1997)
    • (1997) Proceedings Third International Conference on Spacecraft Guidance, Navigation and Control Systems
    • Londerville, G.1
  • 19
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    • Deep impact attitude estimator design and flight performance
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    • Hughes, M. P., Schira, C. N., Deep Impact Attitude Estimator Design and Flight Performance, 29th Annual Guidance and Control Conference, Breckenridge, Colorado, February 2002.paper AAS 06-084
    • (2002) 29th Annual Guidance and Control Conference
    • Hughes, M.P.1    Schira, C.N.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.