Optimal Attitude Sensors Placement for a Solar Power Satellite Considering Control–Structure Interaction-Reference-Cited by-同舟云学术

Optimal Attitude Sensors Placement for a Solar Power Satellite Considering Control–Structure Interaction

Published:2019-10 Issue:10 Volume:57 Page:4593-4598
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zhang Kaiming¹,Wu Shunan¹,Liu Yuliang¹,Wu Zhigang¹

Affiliation:

1. Dalian University of Technology, 116024 Dalian, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference21 articles.

1. Power from the Sun: Its Future

2. Active control technology for large space structures

3. Attitude and Orbit Control of a Very Large Geostationary Solar Power Satellite

4. GlaeseJ. R.McDonaldE. J. “Space Solar Power Multi-Body Dynamics and Controls, Concepts for the Integrated Symmetrical Concentrator Configuration,” NASA TR-NAS8-00151, 2000.

Cited by 7 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. Towards net zero: A technological review on the potential of space-based solar power and wireless power transmission;Heliyon;2024-05

2. Modal frequency identification using the predictor subspace approach for a space solar power station;Journal of Physics: Conference Series;2024-05-01

3. Identification of time-varying inertia tensor parameters of a space solar power satellite based on a robust weighted recursive algorithm under impulsive disturbance;Aerospace Science and Technology;2024-01

4. Towards Net Zero: A Technological Review on the Potential of Space-Based Solar Power and Wireless Power Transmission;2023

5. Recursive identification of inertia tensor parameters of space solar power satellite based on distributed placement of attitude sensors;Aerospace Science and Technology;2022-11