Integrated Kalman Filter for a Flight Control System with Redundant Measurements
Author:
Affiliation:
1. University of Kansas, Lawrence
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2499
Reference15 articles.
1. Figure 14:Body Rates fromIMU. 0 10 20 30 40 50 60 -80 -60 -40 -20 0 20 40 60 80 100 RollRate:FlightData(NAV420)-KF(integrated)-KF(cascade)[deg/sec]
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