Fault Detection and Isolation of Satellite Inertial Instrumentation Using Nonlinear Adaptive Filters-Reference-Cited by-同舟云学术

Fault Detection and Isolation of Satellite Inertial Instrumentation Using Nonlinear Adaptive Filters

Published:2015-02 Issue:2 Volume:12 Page:284-289
ISSN:2327-3097
Container-title:Journal of Aerospace Information Systems
language:en
Short-container-title:Journal of Aerospace Information Systems

Author:

Das Manasi¹,Sadhu Smita¹,Ghoshal T. K.¹

Affiliation:

1. Department of Electrical Engineering, Jadavpur University, Kolkata 700 032, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Electrical and Electronic Engineering,Computer Science Applications,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.I010180

Reference7 articles.

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2. Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter

3. PirmoradiF. “Fault Detection and Diagnosis in a Spacecraft Attitude Determination System,” M.A.Sc. Dissertation, Dept. of Mechanical Engineering, Univ. of British Columbia, Vancouver, 2005.

4. XiongK.ChanC. W.ZhangH. Y. “Detection of Satellite Attitude Sensor Faults Using the UKF,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 43, No. 2, 2007, pp. 480–491. doi:10.1109/TAES.2007.4285348

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