2014
DOI: 10.1016/j.automatica.2014.08.010
|View full text |Cite
|
Sign up to set email alerts
|

Rigid body attitude estimation based on the Lagrange–d’Alembert principle

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
2

Citation Types

3
100
0

Year Published

2015
2015
2022
2022

Publication Types

Select...
5
2

Relationship

3
4

Authors

Journals

citations
Cited by 74 publications
(103 citation statements)
references
References 9 publications
3
100
0
Order By: Relevance
“…Because of these properties of the function Φ, the critical points and their indices coincide for U 0 r and Φ(U 0 r ) [11]. Define the kinetic energy-like function:…”
Section: A Lagrangian From Measurement Residualsmentioning
confidence: 99%
See 3 more Smart Citations
“…Because of these properties of the function Φ, the critical points and their indices coincide for U 0 r and Φ(U 0 r ) [11]. Define the kinetic energy-like function:…”
Section: A Lagrangian From Measurement Residualsmentioning
confidence: 99%
“…where W is positive definite (not necessarily diagonal) which can be selected according to Lemma 3.2 in [11], and Φ :…”
Section: A Lagrangian From Measurement Residualsmentioning
confidence: 99%
See 2 more Smart Citations
“…However, due to the nonlinear nature of the navigation equations, and in particular to the fact the orientation of the aircraft (i.e., the attitude) does not live in a vector space, the EKF may have some shortcomings. This has motivated the development of alternative filters, especially for attitude estimation, see e.g., [12], [19], [6], [15], [13], [10], [16], [20], [7].…”
Section: Introductionmentioning
confidence: 99%