Minimax failure detection and identification in redundant gyro and accelerometer systems.
Author:
Affiliation:
1. MIT, Cambridge, Mass.
2. Charles Stark Draper Laboratory, MIT, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27753
Reference11 articles.
1. Experimental strapdown redundant sensor inertial navigation system
2. A Redundant Strapdown Inertial Reference Unit (SIRU)
3. Maximum likelihood failure detection for redundant inertial instruments
4. An adaptive technique for a redundant-sensor navigation system
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