Minimax failure detection and identification in redundant gyro and accelerometer systems.
- 1 April 1973
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 10 (4), 236-243
- https://doi.org/10.2514/3.27753
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Maximum likelihood failure detection for redundant inertial instrumentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- An adaptive technique for a redundant-sensor navigation systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- A Redundant Strapdown Inertial Reference Unit (SIRU)Journal of Spacecraft and Rockets, 1972
- Experimental strapdown redundant sensor inertial navigation systemJournal of Spacecraft and Rockets, 1970