Attitude solving algorithm and FPGA implementation of four-rotor UAV based on improved mahony complementary filter

Y Zhu, J Liu, R Yu, Z Mu, L Huang, J Chen, J Chen - Sensors, 2022 - mdpi.com
With the development of modern industry, small UAVs have been widely used in agriculture,
mapping, meteorology, and other fields. There is an increasing demand for the core attitude …

Model, control, and realistic visual 3D simulation of VTOL fixed-wing transition flight considering ground effect

E Irmawan, A Harjoko, A Dharmawan - Drones, 2023 - mdpi.com
The research topic of VTOL (vertical take-off and landing) fixed wing (VFW) is gaining
significant attention, particularly in the transition phase from VTOL to fixed wing and vice …

Mobile robot localization via unscented kalman filter

L Lasmadi, F Kurniawan, D Dermawan… - … on Research of …, 2019 - ieeexplore.ieee.org
Mobile robot localization concerns estimating the position and heading of the robot relative
to its environment. Basically, the mobile robot moves around without initial knowledge of the …

[PDF][PDF] Two cross coupled and Madgwicks filter for estimation of multi-channel dividing systems

NA Kadhim, A jawad Alrubaie… - Indonesian Journal of …, 2022 - academia.edu
The estimates of Rayleigh fading channels are rapidly changing in multi carrier direct
sequence code division multiple access (MC-DS-CDMA) multiplexing systems. The most …

Accurate Attitude Control for an Asymmetrical Hexacopter Under Exogenous Disturbance

J Hu, W Zheng, K Liu, Z Qin… - 2022 34th Chinese Control …, 2022 - ieeexplore.ieee.org
The distributed electric propulsion (DEP) vertical take-off and landing (VTOL) drone has the
characteristics of both rotary-wing and fixed-wing aircraft. The dynamic model of its take-off …

Autonomous Take-off Control System with Stall Prevention for Fixed-Wing UAVs Utilizing LQR Method

AM Handayani, A Dharmawan… - 2024 IEEE 33rd …, 2024 - ieeexplore.ieee.org
During the launch sequence of a Fixed-wing Unmanned Aerial Vehicle (UAV), the process
encompasses several phases: taxiing on the ground, ascending, and transitioning to steady …

Auto Landing System on A Fixed Wing Unmanned Aerial Vehicle Using Linear Quadratic Approach

A Dharmawan, A Ashari, AM Handayani… - … on Science and …, 2019 - ieeexplore.ieee.org
The primary control issue on Unmanned Aerial Vehicle (UAV) is to control the rotation
motion in the form of pitch, roll, and yaw. These rotational movements are used for various …