Optimal strapdown attitude integration algorithms-Reference-Cited by-同舟云学术

Optimal strapdown attitude integration algorithms

Published:1990-03 Issue:2 Volume:13 Page:363-369
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Ignagni M. B.¹

Affiliation:

1. Honeywell Systems and Research Center, Minneapolis, Minnesota

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/10.2514/3.20558

Reference5 articles.

1. z, J. "A New Mathematical Formulation for Strapdown Inertial Navigation," IEEE Transactions on Aerospace and Electronic Systems, Vol. AES7, No.1, Jan. 1973.

2. The State of Strapdown Inertial Guidance and Navigation

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