2014
DOI: 10.1016/j.proeng.2014.12.139
|View full text |Cite
|
Sign up to set email alerts
|

Mathematical Modelling and Parameter Identification of Quadrotor (a survey)

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

0
58
1
1

Year Published

2015
2015
2022
2022

Publication Types

Select...
5
2
1

Relationship

0
8

Authors

Journals

citations
Cited by 118 publications
(60 citation statements)
references
References 5 publications
0
58
1
1
Order By: Relevance
“…A fairly thorough derivation of the Newton-Euler formulism for multirotor UAV is provided in Refs. [16] and [17]. Following these formulations, the Newton-Euler UAV dynamics are given by…”
Section: Rotor Frame Dynamicsmentioning
confidence: 99%
“…A fairly thorough derivation of the Newton-Euler formulism for multirotor UAV is provided in Refs. [16] and [17]. Following these formulations, the Newton-Euler UAV dynamics are given by…”
Section: Rotor Frame Dynamicsmentioning
confidence: 99%
“…Multicopters have been received a significant interest in various applications such as rescue missions, inspection of structures, environment monitoring, and military reconnaissance [1], [2]. Advantages of multicopters on mechanical simplicity and high maneuverability enable to conduct advanced missions in academic research and industrial applications with advanced control algorithms.…”
Section: Introductionmentioning
confidence: 99%
“…The methods on multicopter system identification are mainly divided into two different approaches: (i) direct computation of geometry and (ii) analysis from flight data [3]. For instance, CAD models are used to calculate all the missing parameters and the moment of inertia in [1], [4] for direct computation of geometry. In [1], [3], Unscented Kalman Filter (UKF) is implemented to identify and estimate parameters of quadrotors from flight data.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Firstly, RAR system kinetic mechanism is rely on the aerodynamics produced by high-speed revolution of propellers, which results in the obvious nonlinear characteristics, strong coupling, under-actuated feature and high sensitivity to perturbations [4] . The RAMS dynamic complexity further increases owing to the operating mechanism, making system modeling and controller design much more difficult.…”
mentioning
confidence: 99%