Three-Axis Attitude Estimation Using Rate-Integrating Gyroscopes
Author:
Affiliation:
1. University at Buffalo, State University of New York, Amherst, New York 14260-4400
2. NASA Goddard Space Flight Center, Greenbelt, Maryland 20771
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.G000336
Reference18 articles.
1. Survey of Nonlinear Attitude Estimation Methods
2. Strapdown Inertial Navigation Integration Algorithm Design Part 2: Velocity and Position Algorithms
3. Inertial navigation systems for mobile robots
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