2016
DOI: 10.1177/0142331216658947
|View full text |Cite
|
Sign up to set email alerts
|

Finite time attitude tracking control of an autonomous airship

Abstract: The problem of station-keeping attitude tracking control for an autonomous airship with system uncertainties and external disturbances is investigated. Adaptive laws are applied to estimate the upper bounds of uncertainties and disturbances, and a nonlinear finite time control scheme is proposed by combing input/output feedback linearization with integral sliding mode technique. Different from the existing works on attitude control of airship, the developed controller can guarantee the yaw, pitch and roll angl… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
12
0

Year Published

2018
2018
2021
2021

Publication Types

Select...
8
1

Relationship

3
6

Authors

Journals

citations
Cited by 28 publications
(12 citation statements)
references
References 29 publications
0
12
0
Order By: Relevance
“…We can see that (70) is a strict feedback nonlinear MIMO system. The detailed parameters can be found in Wang et al (2016). In the simulation, we assume that f 1 is known while f 2 is unknown.…”
Section: Simulation Studiesmentioning
confidence: 99%
“…We can see that (70) is a strict feedback nonlinear MIMO system. The detailed parameters can be found in Wang et al (2016). In the simulation, we assume that f 1 is known while f 2 is unknown.…”
Section: Simulation Studiesmentioning
confidence: 99%
“…Classified by the applied control techniques, we can roughly see two categories when treating the uncertainty (such as external disturbance): the robust control where we design controller to suppress the unknown uncertainty, and the estimation-based controller where we design a dynamical system to estimate the unknown uncertainty, and compensate it by using the closed-loop controller. For the first category, we can cite the Lyapunov theory based controllers [2,3,4,5,6], the Line of Sight guidance laws for path following [7,8], gain scheduling controllers [9,10], sliding mode controls [11,12], model predictive controls [13,14], etc. For the second type, it is also named as active disturbance rejection control in the literature, which has been applied in [15] to control the horizontal trajectory of an airship.…”
Section: Related Workmentioning
confidence: 99%
“…Therefore, it is of practical significance to design a finite‐time control method for airship trajectory tracking. A finite‐time attitude tracking control of autonomous airship is designed in [41], but the control law is discontinuous and the effect of disturbances is not taken into account. Recently, the backstepping‐SMC is studied to have a good control performance.…”
Section: Introductionmentioning
confidence: 99%