A disaster management specific mobility model for flying ad-hoc network

A Mukherjee, N Dey, N Kausar, AS Ashour… - … tools, and applications, 2019 - igi-global.com
Abstract The extended Mobile Ad-hoc Network architecture is a paramount research domain
due to a wide enhancement of smart phone and open source Unmanned Aerial Vehicle …

Precision landing using an adaptive fuzzy multi-sensor data fusion architecture

MK Al-Sharman, BJ Emran, MA Jaradat, H Najjaran… - Applied soft …, 2018 - Elsevier
The positional inaccuracies associated with the GPS/INS measurements make the terminal
phase of the normal GPS/INS landing system imprecise. To solve this problem, an adaptive …

Symbolic representation and toolkit development of iterated error-state extended kalman filters on manifolds

D He, W Xu, F Zhang - IEEE Transactions on Industrial …, 2023 - ieeexplore.ieee.org
Error-state extended Kalman filter (ESEKF) is one of the extensively used filtering
techniques in robot systems. There are many works that cast ESEKF on manifolds to …

Stabilization of a quadrotor system using an optimal neural network controller

MM Farzaneh, AR Tavakolpour-Saleh - Journal of the Brazilian Society of …, 2022 - Springer
This paper presents a new and practical neural network-based optimal control method for a
quadrotor system. Due to the difficulty in obtaining the exact model of the quadrotor system …

[PDF][PDF] Attitude Estimation for Quadrotor Based on IMU with Kalman-Filter

L Lasmadi - Conference SENATIK STT Adisutjipto Yogyakarta, 2018 - scholar.archive.org
Improved a quadrotor technology that is capable of fast maneuvering requires accurate
attitude estimation or navigation to maintain a quadrotor stability. The GPS can provide …

Extended Kalman Filter and LQR controller design for quadrotor UAVs

MM Raja - 2017 - corescholar.libraries.wright.edu
A quadrotor is a unique class of UAVs with vertical take off and landing (VTOL) capability
and has attracted significant attention due to its importance in various applications. This …

Real-time terrain-following of an autonomous quadrotor by multi-sensor fusion and control

Y Yang, Y Huang, H Yang, T Zhang, Z Wang, X Liu - Applied Sciences, 2021 - mdpi.com
For the application of the autonomous guidance of a quadrotor from confined undulant
ground, terrain-following is the major issue for flying at a low altitude. This study has …

Simulation of Orientation Navigation Based on IMU Sensor for Quadrotor Using Kalman Filter

F Kurniawan, D Dermawan, NA Purnami… - … on Electrical and …, 2023 - ieeexplore.ieee.org
The inertial navigation system (INS) calculates the position, attitude orientation, and speed
of the quadrotor relative to its initial or last known state. This paper aims to validate the …

[PDF][PDF] Design and implementation of hardware in the loop simulation for electric ducted fan rocket control system using 8-bit microcontroller and real-time open source …

RA Yulnandi, C Machbub, AS Prihatmanto… - … , Electrical Power, and …, 2017 - academia.edu
Abstract Hardware in the Loop Simulation (HILS) is intended to reduce time and
development cost of control system design. HILS systems are mostly built by integrating both …

Low-cost quadrotor attitude solution based on improved complementary filtering

P Shang, Y Gao, Z Song - 2018 IEEE 4th Information …, 2018 - ieeexplore.ieee.org
Aiming at the problem that the low-cost inertial measurement device is susceptible to
external disturbance and the accuracy of real-time attitude calculation is poor, an improved …