Robust Adaptive Unscented Kalman Filter for Spacecraft Attitude Estimation Using Quaternion Measurements-Reference-Cited by-同舟云学术

Robust Adaptive Unscented Kalman Filter for Spacecraft Attitude Estimation Using Quaternion Measurements

Published:2017-07 Issue:4 Volume:30 Page:04017009
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lee Daero¹,Vukovich George²,Lee Regina³

Affiliation:

1. Postdoctoral Researcher, Dept. of Earth and Space Science and Engineering, York Univ., 4700 Keele St., Toronto, ON, Canada M3J 1P3 (corresponding author).

2. Associate Professor, Dept. of Earth and Space Science and Engineering, York Univ., Lassonde School of Engineering, 4700 Keele St., Toronto, ON, Canada M3J 1P3.

3. Professor, Dept. of Earth and Space Science and Engineering, York Univ., Lassonde School of Engineering, 4700 Keele St., 150 Atkinson College, Toronto, ON, Canada M3J 1P3.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000718

Reference19 articles.

1. Attitude estimation for satellite fault tolerant system using federated unscented Kalman filter;Bae J.;Int. J. Aeronaut. Space Sci.,2010

2. Unscented Filtering for Spacecraft Attitude Estimation

3. Analytic Steady-State Accuracy Solutions for Two Common Spacecraft Attitude Estimators

4. Robust adaptive unscented Kalman filter for attitude estimation of pico satellites

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