Small-Satellite Attitude Consensus on SO(3) Using Continuous But Only Piecewise-Continuously Differentiable Sinusoidal Controls-Reference-Cited by-同舟云学术

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Small-Satellite Attitude Consensus on SO(3) Using Continuous But Only Piecewise-Continuously Differentiable Sinusoidal Controls

Published:2021-05-25 Issue: Volume: Page:
ISSN:
Container-title:2021 American Control Conference (ACC)
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Author:

Chavan Roshan A.,Seigler T. M.,Hoagg Jesse B.

Funder

National Aeronautics and Space Administration

National Science Foundation

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9482409/9482614/09483055.pdf?arnumber=9483055

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. Small-satellite attitude consensus using limited-stroke oscillating-mass actuators with continuous sinusoidal controls;Aerospace Science and Technology;2023-11

2. Literature Review;Distributed Attitude Consensus of Multiple Flexible Spacecraft;2022-09-18

3. Review of attitude consensus of multiple spacecraft;Astrodynamics;2022-07-09

4. Small-Satellite Attitude Control Using Stroke-Limited Vibrating-Mass Actuators With Piecewise Constant Control Signals;2022 American Control Conference (ACC);2022-06-08

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