Rotation vector and directional cosine matrix in problems of satellite attitude control

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Simple item page

Full item details

creativework.keywords - en

rigid body dynamics

attitude determination and control

Euler angles

quaternion

directional cosine matrix

rotation angles

rotation vector

Euler's axis

dc.contributor.author

Kim, Yuri

dc.date.accessioned

2023-05-19T20:14:21Z

dc.date.available

2023-05-19T20:14:21Z

dc.date.issued

2022-09-16

dc.description.abstract - en

For many years, three rotation angles of moving vehicles: Roll, Pitch, and Yaw have been used for attitude determination and control. However, in the last years due to new airspace applications, such as strapdown Inertial Navigation Systems (INS) and spacecrafts, new quaternion (Q) based methods of classic mechanics appeared in aerospace systems engineering practice. Conventional and new modern methods have some features that can attract or repel developers. Nevertheless, some new techniques of classical mechanics can be tried to use them for vehicle attitude determination and control purposes with the expectation to get more effective results. The article presents a Rotation Vector (RV) and proposes a way of using it for satellite attitude control. This method is compared with conventional method of attitude control using three Rotation Angles. The ratio is shown between RV control and modern method of satellite attitude control using quaternion. Analytical and simulation results are presented.

dc.identifier.citation

Y.V. Kim, (2022) ‘Rotation Vector and Directional Cosine Matrix in problems of satellite attitude control’, Int. J. Space Science and Engineering, Vol. 20, No. 5.

dc.identifier.doi

https://doi.org/10.1504/IJASSE.2021.10036566

dc.identifier.uri

https://open-science.canada.ca/handle/123456789/294

dc.language.iso

en

dc.publisher

Inderscience Publishers

dc.subject - en

Science and technology

dc.subject - fr

Sciences et technologie

dc.subject.en - en

Science and technology

dc.subject.fr - fr

Sciences et technologie

dc.title - en

Rotation vector and directional cosine matrix in problems of satellite attitude control

dc.type - en

Submitted manuscript

dc.type - fr

Manuscrit soumis

local.article.journalissue

5

local.article.journaltitle

International Journal of Space Science and Engineering

local.article.journalvolume

20

local.pagination

1-23