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Volumn 3, Issue 5, 2003, Pages 569-578

Common design techniques for BEI gyrochip* quartz rate sensors for both automotive and aerospace/defense markets

Author keywords

GyroChip; Microelectromechanical systems (MEMS) gyroscope; Quartz rate sensor (QRS); Yaw sensor

Indexed keywords

AEROSPACE ENGINEERING; AUTOMOTIVE ENGINEERING; GYROSCOPES; MICROELECTROMECHANICAL DEVICES; MILITARY ROCKETS; MISSILES; PRODUCT DESIGN; QUARTZ;

EID: 3042823724     PISSN: 1530437X     EISSN: None     Source Type: Journal    
DOI: 10.1109/JSEN.2003.817728     Document Type: Article
Times cited : (68)

References (11)
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  • 3
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    • A micro-electromechanical quartz rotational rate sensor for inertial applications
    • Feb.
    • A. M. Madni, L. A. Wan, and S. Hammons, "A micro-electromechanical quartz rotational rate sensor for inertial applications," Proc. IEEE Aerospace Applications Conf., vol. 2, pp. 315-332, Feb. 1996.
    • (1996) Proc. IEEE Aerospace Applications Conf. , vol.2 , pp. 315-332
    • Madni, A.M.1    Wan, L.A.2    Hammons, S.3
  • 5
    • 1542345217 scopus 로고    scopus 로고
    • A third generation, highly monitored, micromachined quartz yaw rate sensor for safety-critical automotive stability control
    • Mar.
    • A. M. Madni and L. E. Costlow, "A third generation, highly monitored, micromachined quartz yaw rate sensor for safety-critical automotive stability control," in Proc. IEEE Aerospace Conf., Mar. 2001, pp. 2523-2534.
    • (2001) Proc. IEEE Aerospace Conf. , pp. 2523-2534
    • Madni, A.M.1    Costlow, L.E.2
  • 7
    • 3042771095 scopus 로고    scopus 로고
    • Aerospace technology and low automotive costs benefit quartz micromachined gyros
    • June. Session B1, Paper no. 4
    • A. M. Madni, L. E. Costlow, and R. P. Jaffe, "Aerospace technology and low automotive costs benefit quartz micromachined gyros," in Proc. Inst. Navigation 57th Annu. Meeting, June 2001. Session B1, Paper no. 4.
    • (2001) Proc. Inst. Navigation 57th Annu. Meeting
    • Madni, A.M.1    Costlow, L.E.2    Jaffe, R.P.3
  • 8
    • 3042817677 scopus 로고
    • "Rotation Rate Sensor With Built in Test Circuit," U.S. patent 5 426 970, June
    • A. Florida, P. Gupta, D. Macy, and H. Morris, "Rotation Rate Sensor With Built in Test Circuit," U.S. patent 5 426 970, June 1995.
    • (1995)
    • Florida, A.1    Gupta, P.2    Macy, D.3    Morris, H.4
  • 9
    • 3042853456 scopus 로고
    • "Rotation Rate Sensor With Center Mounted Tuning Fork," U.S. patent 5 396 144, Mar. 7
    • P. K. Gupta and C. E. Jenson, "Rotation Rate Sensor With Center Mounted Tuning Fork," U.S. patent 5 396 144, Mar. 7, 1995.
    • (1995)
    • Gupta, P.K.1    Jenson, C.E.2
  • 10
    • 3042733790 scopus 로고    scopus 로고
    • "Inertial Rate Sensor Tuning Fork," U.S. patent 6 262 520 B1, July 17
    • S. J. Knowles, "Inertial Rate Sensor Tuning Fork," U.S. patent 6 262 520 B1, July 17, 2001.
    • (2001)
    • Knowles, S.J.1
  • 11
    • 3042817676 scopus 로고    scopus 로고
    • Full circle commercialization of a quartz rate sensor: Aerospace to automotive to aerospace
    • Ypsilanti, MI, Sept. 8-12
    • A. M. Madni, L. E. Costlow, and J. LaBoskey, "Full circle commercialization of a quartz rate sensor: Aerospace to automotive to aerospace," in Proc. COMS, Ypsilanti, MI, Sept. 8-12, 2002, pp. 443-451.
    • (2002) Proc. COMS , pp. 443-451
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.