Results 1 to 10 of about 623 (226)

Robust Preview Control and Autoregressive Prediction for Aircraft Automatic Carrier Landing [PDF]

open access: yesIEEE Access, 2019
This paper studies an automatic carrier landing control problem of fixed-wing aircraft with system uncertainties under the airwake and deck motion disturbances.
Ziyang Zhen   +3 more
doaj   +2 more sources

Backstepping- and Sliding Mode-Based Automatic Carrier Landing System with Deck Motion Estimation and Compensation

open access: yesAerospace, 2022
This paper addresses the automatic carrier landing problem in the presence of deck motion, carrier airwake disturbance, wind shears, wind gusts, and atmospheric turbulences.
Mihai Lungu   +2 more
doaj   +3 more sources

ADRC-Based UAV Control Scheme for Automatic Carrier Landing

open access: yesEngineering Proceedings, 2023
In this paper the problem of atmospheric disturbances during the UAV carrier landing operation is considered. A UAV dynamics model, and a wind gust and airwake disturbance model are introduced.
Ruiyang Zhou, Konstantin A. Neusypin
doaj   +2 more sources

Model Predictive Control for Automatic Carrier Landing with Time Delay

open access: yesInternational Journal of Aerospace Engineering, 2021
This paper focuses on the problem of automatic carrier landing control with time delay, and an antidelay model predictive control (AD-MPC) scheme for carrier landing based on the symplectic pseudospectral (SP) method and a prediction error method with ...
Kaikai Cui   +5 more
doaj   +2 more sources

Design of Automatic Carrier-Landing Controller Based on Compensating States and Dynamic Inversion [PDF]

open access: yesIEEE Access, 2019
In this paper, a design scheme of automatic carrier landing system (ACLS) control law based on compensating states and dynamic inversion is proposed, in order to eliminate landing risk and air wake disturbance and improve flight quality during landing ...
Lipeng Wang   +3 more
doaj   +2 more sources

Impact of visual guidance error on automatic carrier landing performance

open access: yesHangkong gongcheng jinzhan
The positioning accuracy of guidance system is the key factor of automatic carrier landing system to determine the success or failure of the carrier landing.
ZHEN Chong   +4 more
doaj   +2 more sources

Analysis of Security Window in Automatic Landing of the Carrier-borne Aircraft

open access: yesResearch Journal of Applied Sciences, Engineering and Technology, 2014
Wave-off judgment research of carrier-borne aircraft in the landing process led by automatic landing system is made and the conception of security window in automatic Landing of the carrier-borne aircraft is proposed. Through the study of carrier-borne aircraft's landing process under the guidance of automatic landing system, considering on the impact ...
Han Zhimin, Hong Guanxin
exaly   +2 more sources

Carrier Aircraft Flight Controller Design by Synthesizing Preview and Nonlinear Control Laws

open access: yesDrones, 2023
This paper proposes an innovative automatic carrier landing control law for carrier-based aircraft considering complex ship motion and wind environment. Specifically, a strategy is proposed to synthesize preview control with an adaptive nonlinear control
Baoxu Jia   +5 more
doaj   +1 more source

Simulation and Analysis of Approach Power Compensation for Automatic Landing with Carrier Air Wake [PDF]

open access: yesHangkong bingqi, 2023
In the process of carrier landing, the carrier air wake affects the height and speed of carrier aircraft, resulting in landing deviation and even going around. Aiming at the problem of poor accuracy of landing point caused by carrier air wake, this paper
Huang Xudong, Zhu Wanbo, Wen Zixia, Liu Wei
doaj   +1 more source

Automatic landing on aircraft carrier by visual servoing [PDF]

open access: yes2011 IEEE/RSJ International Conference on Intelligent Robots and Systems, 2011
The landing on carrier is a very difficult task even for trained pilots. This paper presents a method to land automatically using aircraft sensors and three visual features inspired by visual cues used by pilots. These features whose link with the aircraft state is established, are introduced in a control scheme using a linearized aircraft model.
Coutard, L.   +2 more
openaire   +2 more sources

Home - About - Disclaimer - Privacy