2018
DOI: 10.5302/j.icros.2018.18.0025
|View full text |Cite
|
Sign up to set email alerts
|

Rotation Matrix Attitude Update Method For 3D Flight Control

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
2

Relationship

0
2

Authors

Journals

citations
Cited by 2 publications
(2 citation statements)
references
References 0 publications
0
2
0
Order By: Relevance
“…Finally, the problem of the forward solution of the shield pose can be considered as the problem of finding the roots of Equation (15). However, obtaining an analytical solution is challenging because Equation ( 15) is a multivariate nonlinear equation with multiple solutions.…”
Section: Forward Kinematic Modelmentioning
confidence: 99%
“…Finally, the problem of the forward solution of the shield pose can be considered as the problem of finding the roots of Equation (15). However, obtaining an analytical solution is challenging because Equation ( 15) is a multivariate nonlinear equation with multiple solutions.…”
Section: Forward Kinematic Modelmentioning
confidence: 99%
“…The Euler angles (Z-Y-X) in robotics are adopted to describe the attitude of the shield machine relative to the coordinate frame {A}. Thus, the rotation matrix can be written as Equation (2) [25,26]:…”
Section: Rotation Matrix and Euler Anglesmentioning
confidence: 99%