A 3-DoF Experimental Test-Bed for Integrated Attitude Dynamics and Control Research-Reference-Cited by-同舟云学术

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A 3-DoF Experimental Test-Bed for Integrated Attitude Dynamics and Control Research

Published:2003-06-22 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
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Author:

Jung Dongwon¹,Tsiotras Panagiotis¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5331

Reference14 articles.

1. 10 20 30 40 50 -1500 : Experiment : Simulation

2. 10 20 30 40 50 -4000 -3000 -2000 -1000

3. 10 20 30 40 50 -4000 -3000 -2000 -1000

Cited by 19 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. Automatic Mass Balancing of a Small Spherical Simulator for Attitude Control Verification;IEEE Access;2024

2. Adaptive control for excitation and parameter identification of a three-axis spacecraft simulator with full-state constraints;Aerospace Systems;2023-07-20

3. Spin-Stabilization and Attitude Tracking of a Spacecraft Simulator using MPC;AIAA SCITECH 2023 Forum;2023-01-19

4. A review of balancing methods for satellite simulators;Acta Astronautica;2021-10

5. A suboptimal excitation torque for parameter estimation of a 5-DOF spacecraft simulator;Advances in Space Research;2018-11

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