Nonlinear Model Predictive Control of a 6DOF Spacecraft on Lie Group SE(3)-Reference-Cited by-同舟云学术

Nonlinear Model Predictive Control of a 6DOF Spacecraft on Lie Group SE(3)

Published:2023-07-14 Issue: Volume: Page:
ISSN:
Container-title:2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA)
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Author:

Li Zijian¹,Wang Hai²,Xu Shidong³

Affiliation:

1. Nanjing university of Aeronautics and Astronautics,College of Aerospace Engineering,Nanjing,Jiangsu,P. R. China,210016

2. PipeChina West East Gas Pipeline Company,Shanghai,P. R. China,200122

3. Nanjing university of Aeronautics and Astronautics,State Key Laboratory of Mechanics and Control for Aerospace Structures,Nanjing,Jiangsu,P. R. China,210016

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Fundamental Research Funds for the Central Universities

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10243163/10243123/10243314.pdf?arnumber=10243314

Reference19 articles.

1. A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon

2. Lie group variational integrators for the full body problem in orbital mechanics

3. A Lie group variational integrator for rigid body motion in SE(3) with applications to underwater vehicle dynamics;nordkvist;Proceedings of IEEE Conference on Decision and Control,2011

4. Discrete mechanics and variational integrators

5. A Lie group variational integrator for the attitude dynamics of a rigid body with applications to the 3D pendulum;lee;Proceedings of IEEE Conference on Control Applications,2005

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