To read this content please select one of the options below:

Lateral autonomous carrier-landing control with high-dimension landing risks consideration

Lipeng Wang (College of Automation, Harbin Engineering University, Harbin, China)
Zhi Zhang (College of Automation, Harbin Engineering University, Harbin, China)
Qidan Zhu (College of Automation, Harbin Engineering University, Harbin, China)
Xingwei Jiang (Shanghai Avionics Corporation, Shanghai, China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 27 April 2020

174

Abstract

Purpose

This paper aims to propose a novel model predictive control (MPC) with time varying weights to develop a lateral control law in an automatic carrier landing system (ACLS), which minimizes landing risk and improves flight quality.

Design/methodology/approach

First, a nonlinear mathematic model of an F/A-18 aircraft during lateral landing is established. Then the landing model is linearized in the form of state deviations on the equilibrium points. Second, landing risk windows are proposed and a high-dimensional landing risk model is addressed through a back propagation (BP) neural network. The trained samples are acquired based on a pilot behavior model. Third, time varying weights created from the lateral landing risk are introduced into the performance function of MPC. Optimal solution is solved quicker and some state deviations are focused on and eliminated. Fourth, the algebraic inequalities are substituted by the linear matrix inequalities (LMIs), which are easily calculated by the computers.

Findings

On a semi-physical platform, the proposed method compares with a traditional MPC algorithm and a modified MPC with an additional term. The test results indicate that the proposed algorithm brings about an excellent landing performance as well as an ability of eliminating landing risk.

Practical implications

The landing phase of a carrier-based aircraft is one of the most dangerous and complicated stages, and the algorithm proposed by this paper plays a vital role in the lateral landing.

Originality/value

This paper establishes a lateral landing risk model, which considers not only the current landing state but also the future touchdown point. This lateral landing risk is integrated into the time varying weights of the MPC algorithm so that the state deviations and landing risk can be both reduced in the rolling optimization.

Keywords

Acknowledgements

This work was supported by the National Natural Science Foundation of China (No. 61803116) and the Fundamental Research Funds for the Central Universities of China (No. 3072019CFJ0405).

Citation

Wang, L., Zhang, Z., Zhu, Q. and Jiang, X. (2020), "Lateral autonomous carrier-landing control with high-dimension landing risks consideration", Aircraft Engineering and Aerospace Technology, Vol. 92 No. 6, pp. 837-850. https://doi.org/10.1108/AEAT-06-2019-0134

Publisher

:

Emerald Publishing Limited

Copyright © 2020, Emerald Publishing Limited

Related articles