Estimation of a Spacecraft's Attitude Dynamics Parameters by Using Flight Data-Reference-Cited by-同舟云学术

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Estimation of a Spacecraft's Attitude Dynamics Parameters by Using Flight Data

Published:2005-07 Issue:4 Volume:28 Page:594-603
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Psiaki Mark L.¹

Affiliation:

1. Cornell University, Ithaca, New York 14853-7501

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.7362

Reference19 articles.

1. Three-axis attitude determination via Kalman filtering of magnetometer data

2. ALEXIS Spacecraft Attitude Reconstruction with Thermal/Flexible Motions Due to Launch Damage

3. Attitude Estimation for a Flexible Spacecraft in an Unstable Spin

4. Magnetometer-only attitude and rate estimates for spinning spacecraft

5. Spacecraft Attitude Rate Estimation from Geomagnetic Field Measurements

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