A solution for the attitude determination of three-vehicle heterogeneous formations-Reference-Cited by-同舟云学术

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A solution for the attitude determination of three-vehicle heterogeneous formations

Published:2019-10 Issue: Volume:93 Page:105275
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cruz Pedro,Batista Pedro

Funder

FCT

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference20 articles.

1. Fundamentals of Spacecraft Attitude Determination and Control;Markley,2014

2. A passive system for determining the attitude of a satellite;Black;AIAA J.,1964

3. A least-squares estimate of satellite attitude;Wahba;SIAM Rev.,1965

4. Three-axis attitude determination from vector observations;Shuster;J. Guid. Control Dyn.,1981

5. Fast linear quaternion attitude estimator using vector observations;Wu;IEEE Trans. Autom. Sci. Eng.,2017

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design and analysis of attitude observers based on the Lagrange-d’Alembert principle applied to constrained three-vehicle formations;Advances in Space Research;2022-06

2. Attitude Uncertainty Analysis of a Three-Vehicle Constrained Formation;Sensors;2022-05-20

3. Characterization of Degenerate Configurations in Attitude Determination of Three-Vehicle Heterogeneous Formations;Sensors;2021-07-06

4. Attitude observers for three-vehicle heterogeneous formations based on the Lagrange-d’Alembert principle;2021 European Control Conference (ECC);2021-06-29

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