Test and evaluation of high performance micro electro-mechanical system based inertial measurement units

Record - IEEE PLANS, Position Location and Navigation Symposium

Volumn 2006, Issue , 2006, Pages 405-414

  Pethel, Stephen J ^a  

^a Navigation Technology Associates   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GUIDED MUNITIONS; INERTIAL MEASUREMENT UNITS (IMU); MISSILE PLATFORMS;

ELECTRONIC EQUIPMENT TESTING; ELECTRONIC GUIDANCE SYSTEMS; MICROSENSORS; MISSILES; PERSONAL COMPUTERS; VIBRATION CONTROL;

MICROELECTROMECHANICAL DEVICES;

EID: 33845576398     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/PLANS.2006.1650630     Document Type: Conference Paper

References (4)

1. "Synchronous Data Link Control: Concepts", IBM Publication No. GA27-3093-04, 5th Edition, May 1992.
2. L. Ng and D. Pines, "Characterization of RLG Performance Using the Allan Variance Method", AIAA Journal of Guidance, Control, and Dynamics, Vol. 20, No. 1, February 1997.
3. Lockheed Martin Corporation, "Inertial Measurement Unit (IMU) Performance Specification," Drawing No. 79749320X, Rev A, January 2005.
4. V. Lefevre and C. Roberts, "Common Guidance Common Sense Phase 2 IMU Temperature Soak Testing", Technical Report NTA-1202-413-05, December 2005, unpublished.