Single axis pointing for underactuated spacecraft with a residual angular momentum-Reference-Cited by-同舟云学术

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Single axis pointing for underactuated spacecraft with a residual angular momentum

Published:2022-05 Issue: Volume:124 Page:107512
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Avanzini Giulio^ORCID,Zavoli Alessandro^ORCID,De Matteis Guido^ORCID,Giulietti Fabrizio

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. Quaternion feedback for spacecraft large angle maneuvers;Wie;J. Guid. Control Dyn.,1985

2. Spacecraft attitude control using magnetic and mechanical actuation;De Angelis;J. Guid. Control Dyn.,2016

3. Single-axis pointing of an underactuated spacecraft equipped with two reaction wheels;Zavoli;J. Guid. Control Dyn.,2017

4. Constrained slews for single-axis pointing;Avanzini;J. Guid. Control Dyn.,2008

5. Single-axis pointing of underactuated spacecraft in the presence of path constraints;De Angelis;J. Guid. Control Dyn.,2015

Cited by 2 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. Hierarchical attitude stabilization controller design and analysis for underactuated spacecraft on SO(3);Aerospace Science and Technology;2024-12

2. Model Predictive Control-Based Attitude Control of Under-Actuated Spacecraft Using Solar Radiation Pressure;Aerospace;2022-09-07

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