[HTML][HTML] A comprehensive survey on the methods of angle of attack measurement and estimation in UAVs

L Sankaralingam, C Ramprasadh - Chinese Journal of Aeronautics, 2020 - Elsevier
Angle of Attack (AOA) is a crucial parameter which directly affects the aerodynamic forces of
an aircraft. The measurement of AOA is required to ensure a safe flight within its designed …

Data driven aerodynamic modeling using Mamdani fuzzy inference systems

AK Sharma, D Singh, NK Verma - … International conference on …, 2018 - ieeexplore.ieee.org
In this paper, an application of Mamdani fuzzy model has been presented for aerodynamic
modeling of the fixed wing aircraft. Here, Mamdani model is used to represent the nonlinear …

Fuzzy Modeling Framework Using Sector Non-Linearity Techniques for Fixed-Wing Aircrafts

P Brusola, S Garcia-Nieto, JV Salcedo, M Martinez… - Aerospace, 2024 - mdpi.com
This paper presents a mathematical modeling approach utilizing a fuzzy modeling
framework for fixed-wing aircraft systems with the goal of creating a highly desirable …

People counting with overhead camera using fuzzy-based detector

NK Verma, R Dev, S Maurya, NK Dhar… - … Theories, Applications and …, 2019 - Springer
This paper presents a novel fuzzy-based detector for overhead people counting in real-time
using RGB camera. The approach, first, extracts the foreground from the subsequent frames …

Stabilization enhancement of the ball on the plate system (BOPS) based on Takagi-Sugeno (TS) fuzzy modeling

MR Elshamy, E Nabil, AS Abdelmageed… - 2021 International …, 2021 - ieeexplore.ieee.org
After applying the ball on plate stabilization system in practice, a big problem appeared,
which is that the servo motors used must be very fast and have large-angle but these motors …

On Consistent Filter Design for Angle of Attack Estimation with Airspeed Rate Measurement

S Huang, F Xiang, W Xue… - 2023 IEEE 12th Data …, 2023 - ieeexplore.ieee.org
This paper is concerned with the problem of estimating the angle of attack (AOA) of the
aircraft. The aerodynamics model of airspeed under constant wind disturbances and the …