Design and experiment of MIMS/GPS integrated navigation system

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 24, Issue 3, 2003, Pages 269-272

  Gu, Qi Tai ^a   Shang, Jie ^a   Mao, Gang ^a   Liu, Xue Bin ^a  

^a TSINGHUA UNIVERSITY   (China)

Author keywords

Global positioning system; Integrated system; Micro miniature inertial measurement system

Indexed keywords

ERROR COMPENSATION; GLOBAL POSITIONING SYSTEM; MINIATURE INSTRUMENTS; VEHICLE LOCATING SYSTEMS;

ANTI INTERFERENCE ABILITY; BIAS FEEDBACK COMPENSATION; INTEGRATED SYSTEM; MICRO MINIATURE INERTIAL MEASUREMENT SYSTEM; POSITIONING ACCURACY;

INERTIAL NAVIGATION SYSTEMS;

EID: 0346778467     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. Silva R N, Murray G W. Low cost quartz rate sensors applied to tactical guidance IMUs [A]. Proceedings of the IEEE Position, Location and Navigation Symposium [C]. 1994. 37-42.
2. Brown R A. Instantaneous GPS attitude determination [A]. Proceedings of the IEEE Position, Location and Navigation Symposium [C]. 1992. 113-120.
3. Li R. A super-fast integer ambiguity resolution approach to GPS interferometric heading determination for the application in a low cost integrated GPS/inertial navigation system [A]. Proceedings of the National Technical Meeting [C]. 1996. 83-88.
4. Friedland B. Treatment of bias in recursive filtering [J]. IEEE Trans on Automatic Control, 1969, AC-14: 359-367.
5. Ignagni M B. An alternate derivation and extension of Friedland's two-state Kalman estimator [J]. IEEE Trans on Automatic Control, 1981, AC-26: 746-750.