Robust modification of nonlinear L1 adaptive flight control system via noise attenuation

Y Feng, Y Wang, Z Sun, B ** - Acta Aeronautica et Astronautica Sinica, 2024 - sciopen.com
This paper systematically sorts out the development status of aviation navigation guidance
and control technology at home and abroad, and analyzes the existing gaps and reasons …

[HTML][HTML] 舰载机自动着舰引导与控制综述

张志冰, 甄子洋, 江驹, 薛艺璇 - 南京航空航天大学学报, 2018 - jnuaa.nuaa.edu.cn
引导与控制是舰载机自动着舰的关键技术, 为此本文对该技术进行综述. 给出了舰载机进场航线
和几种着舰工作模式, 概述了基于跟踪雷达的着舰引导系统和基于卫星的着舰引导系统的工作 …

A Nonlinear Adaptive Autopilot for Unmanned Aerial Vehicles Based on the Extension of Regression Matrix

Q Hu, Y Feng, L Wu, B ** - Drones, 2023 - mdpi.com
In applications of the L 1 adaptive flight control system, we found two limitations to be
extended:(1) the system cannot meet the demands of engineering in terms of nonlinearity …

Longitudinal inner loop flight controller design by using L1 adaptive control theory

Y Yan, W Dong, Q Zou, W **e… - 2015 IEEE International …, 2015 - ieeexplore.ieee.org
In the following paper, L1 adaptive control theory is used to design a controller for
longitudinal short-period aircraft pitch. This controller accounts for the uncertainties of the …

Research on Lateral Unmatched Nonlinear Control of UAV Based on L1 Adaptive Control Theory

L Wang, S Zhang, D Wang - Asia-Pacific International Symposium on …, 2023 - Springer
Aiming at the dimension unmatched in the lateral nonlinear control of UAV system, and the
problems of high-frequency oscillation and uncertainty caused by high adaptive gain in the …

L1 adaptive output feedback controller for tilt-rotor aircraft

K Lu, C Liu, Z Wang, W Wang - 2016 IEEE Chinese Guidance …, 2016 - ieeexplore.ieee.org
This paper considers application of L 1 adaptive output feedback controller to tilt-rotor
aircraft longitudinal autopilot design. The proposed adaptive controller has satisfactory …