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Preview Control and Particle Filtering for Automatic Carrier Landing

IEEE Transactions on Aerospace and Electronic Systems, 2018
This paper studies the automatic carrier landing control problem of aircrafts with the system dynamics of nonlinearity and multivariable coupling, by applying preview control scheme. An automatic carrier landing system is developed, including a particle filtering based flight deck motion prediction, a corrected reference glide slope generation and an ...
Shuoying Jiang, Ju Jiang, Ziyang Zhen
exaly   +3 more sources

Development of the F/A-18A automatic carrier landing system

Journal of Guidance, Control, and Dynamics, 1985
The F/A-18A Automatic Carrier Landing System integrates the aircraft flight control system, throttle control system, inertial navigation sensors, and shipboard SPN-42 tracking radar and computer system to achieve fully automatic approach control to the carrier deck in all weather conditions.
J.M. Urnes, R.K. Hess
exaly   +2 more sources

A multivariable adaptive control scheme for automatic carrier landing of UAV

Aerospace Science and Technology, 2019
Abstract This paper studies a multivariable model reference adaptive control (MRAC) scheme for the automatic carrier-landing control problem of unmanned aerial vehicles (UAVs) with system dynamics of nonlinearity, multivariable coupling and parametric uncertainty. A complete automatic carrier landing system (ACLS) for carrier-based UAVs is developed,
Yixuan Xue, Ziyang Zhen, Gang Tao
exaly   +2 more sources

Automatic Carrier Landing System With Fixed Time Control

IEEE Transactions on Aerospace and Electronic Systems, 2022
Yang Yuan, Haibin Duan, Zhigang Zeng
exaly   +3 more sources

The top-level design study for the automatic carrier landing system

2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC), 2016
This paper focused on the top-level design of the automatic carrier landing system. The carrier platform and carrier-based aircraft landing technology in China have been mature and stable now, in this case, to develop the automatic carrier landing system and to put it into use will greatly enhance the operational capability of the aircraft carrier.
null Lu Keke   +2 more
exaly   +2 more sources

Image-Based Visual Servoing Control for Automatic Carrier Landing

2021 40th Chinese Control Conference (CCC), 2021
This paper studies the control problem of automatic carrier landing for a fixed-wing aircraft through image-based visual servoing (IBVS) technology. An image-aircraft integration model is established by incorporating the virtual image feature into the aircraft dynamics. Based on the model, we established a control framework with the attitude control as
Simin Liu   +3 more
openaire   +1 more source

Robust control design of an automatic carrier landing system

Astrodynamics Conference, 1992
A robust controller, utilizing Hoo control design techniques, is developed for an automatic carrier landing system. First, a detailed nonlinear aircraft simulation, which -includes the aircraft dynamics, pitch attitude autopilot, and automatic thrust compensator, is summarized.
JOHN CRASSIDIS, D. MOOK
openaire   +1 more source

Automatic landing on carrier method of unmanned air vehicle

Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference, 2014
Automated carrier landing of an Unmanned Air Vehicle is a complex process. To successfully complete the task of landing on carrier, firstly the guidance system should give UAV flight control system a proper landing trajectory, then the flight control system according to the instructions given by the guidance system of UAV make the UAV fly on the right ...
Lu Ke, Wang Zhengzhong, Yuan Suozhong
openaire   +1 more source

Control Barrier Function Based Nonlinear Controller for Automatic Carrier Landing

2020 16th International Conference on Control, Automation, Robotics and Vision (ICARCV), 2020
This paper proposes a novel control barrier function(CBF) based output constraints path following control method, which is applied to automatic carrier landing system. The 6 degrees-of-freedom of aircraft model is converted to an affine model. Based on the transformed affine model, backstepping is used as the main control frame.
Haitong Zhou   +3 more
openaire   +1 more source

Improved noise rejection in automatic carrier landing systems

Journal of Guidance, Control, and Dynamics, 1992
A technique for reducing the effect of sensor noise in a closed-loop control system is developed. The effect of radar noise on an automatic carrier landing system is studied using digital computer simulation techniques. A noise rejection filter, which blends model estimates of the plane’s vertical velocity and acceleration with altitude information ...
D. Joseph Mook   +3 more
openaire   +1 more source

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