Aircraft's Approach Integrated Navigation System INS/GNSS Based on Joint Application of Linear and Nonlinear Filtering-Reference-Cited by-同舟云学术

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Aircraft's Approach Integrated Navigation System INS/GNSS Based on Joint Application of Linear and Nonlinear Filtering

Published:2011-01 Issue:1 Volume:44 Page:1866-1871
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Benzerrouk H.,Nebylov A.V.

Publisher

Elsevier BV

Subject

General Medicine

Reference15 articles.

1. Fellow, IEEE, and Tim Bailey,2006

2. Guaranteed Estimation of Signals with Bounded Variances of Derivatives;Kulakova,2005

3. Strapdown Inertial Navigation Integration Algorithm Design Part 1: Attitude Algorithms;Savage;Journal of Guidance, Control, and Dynamics,1998

4. Design of derivative free smothers and predictors;Simandl,2006

5. “Aided Inertial Navigation Systems for Autonomous Land Vehicles,”;Sukkarieh,1999

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1. Vibration Isolation System with Kalman Filter Estimated Acceleration Feedback: An Approach of Negative Stiffness Control;Journal of Sensors;2021-12-16

2. Measurement of aircraft approach using airfield image;Measurement;2019-07

3. Partial ambiguity resolution with integrity risk constraint for high-performance Global Navigation Satellite System navigation;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2013-11-21

4. Robust Nonlinear Filtering Applied to Integrated Navigation System INS/GNSS under Non Gaussian Measurement noise effect;IFAC Proceedings Volumes;2012

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