Fault tolerant integrated radar/inertial altimeter based on Nonlinear Robust Adaptive Kalman filter

Author:

Hajiyev Chingiz

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Integrated Navigation and Guidance Systems;Biezad,1999

2. Introduction to Random Signals and Applied Kalman Filtering;Brown,1992

3. Improving adaptive Kalman estimation in GPS/INS integration;Ding;The Journal of Navigation,2007

4. E. Foxlin, Inertial head-tracker sensor fusion by a complementary separate-bias Kalman filter, in: IEEE Proceedings of VRAIS ʼ96, 1996, pp. 185–195.

5. R.A. Gray, P.S. Maybeck, Integrated GPS/INS/BARO and radar altimeter system for aircraft precision approach landings, in: Proc. of the IEEE National Aerospace and Electronics Conference, Part 1, Dayton, KY, USA, 1995.

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