A GNSS/IMU-Based 5-Hole Pitot Tube Calibration Algorithm

Author:

Sun Kerry1,Regan Christopher D.1,Gebre-egziabher Demoz1

Affiliation:

1. University of Minnesota, Twin Cities

Publisher

American Institute of Aeronautics and Astronautics

Reference51 articles.

1. An airborne experimental test platform: From theory to flight

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3. Combining model-free and model-based angle of attack estimation for small fixed-wing UAVs using a standard sensor suite

4. GNSS/INS based estimation of air data and wind vector using flight maneuvers

5. Larson, T. J. “Evaluation of a Flow Direction Probe and a Pitot-Static Probe on the F-14 Airplane at High Angles of Attack and Sideslip,” Tech. Rep. 84911, NASA Ames Research Center, Dryden FlightResearch Facility, Edwards, California,1984.

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2. Air data fault detection and isolation for small UAS using integrity monitoring framework;NAVIGATION;2021-09

3. Two-Stage Batch Algorithm for Nonlinear Static Parameter Estimation;Journal of Guidance, Control, and Dynamics;2020-05

4. A Fault Detection and Isolation Design for a Dual Pitot Tube Air Data System;2020 IEEE/ION Position, Location and Navigation Symposium (PLANS);2020-04

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