Extended Kalman Filtering for Satellite Orbital Attitude Estimation Based on Gibbs Vector-Reference-Cited by-同舟云学术

Extended Kalman Filtering for Satellite Orbital Attitude Estimation Based on Gibbs Vector

Published:2004-05 Issue:3 Volume:27 Page:509-511
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Lin YuRong¹,Deng ZhengLong¹

Affiliation:

1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China

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/10.2514/1.10338

Reference11 articles.

1. 1Zhang RenWei, Satellite Orbital Attitude Dynamics and Control, Beijing Univ. of Aeronautics and Astronautics Press, Beijing, China, 1998, pp.137-222.

2. Kalman Filtering for Spacecraft Attitude Estimation

3. An attitude determination algorithm for a spacecraft using nonlinear filter

4. Estimation of Rodrigues parameters from vector observations

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