Design and implementation of a compact rotational speed and air flow sensor for unmanned aerial vehicles

F Fries, SKH Win, E Tang, JE Low, LST Win… - IEEE Sensors …, 2019 - ieeexplore.ieee.org
Unmanned aerial vehicles (UAV) have gained massive interest due to their wide range of
applications. In this work, we focus on the design of compact rotation speed sensors (RSS) …

Design, control, aerodynamic performances, and structural integrity investigations of compact ducted drone with co-axial propeller for high altitude surveillance

SS Jayakumar, IP Subramaniam… - Scientific Reports, 2024 - nature.com
Compact multi-rotor unmanned aerial vehicles (UAVs) can be operated in many challenging
environmental conditions. In case the UAV requires certain considerations in designing like …

Applied flight dynamics modeling and stability analysis of a nonlinear time-periodic mono-wing aerial vehicle

FF Ahranjani, A Banazadeh - Aerospace Science and Technology, 2021 - Elsevier
This paper presents fly-ability, trim-ability, stability, and control ability of a mono-wing aerial
vehicle as an under-actuated multi-body system. A nonlinear mathematical model of this …

Orientation filter and angular rates estimation in monocopter using accelerometers and magnetometer with the extended kalman filter

TS Lembono, JE Low, LST Win… - … on Robotics and …, 2017 - ieeexplore.ieee.org
In monocopter flight, two important parameters are required for control: angular rates and
heading direction. Small monocopters fly at a very high speed (more than 600rpm), which …

[PDF][PDF] Shyam Sundar Jayakumar, Indira Prasanth Subramaniam, Beena Stanislaus Arputharaj 2, Senthil Kumar Solaiappan, Parvathy Rajendran 3, It Ee Lee 4Ε …

RK Gnanasekaran, A Karuppasamy, V Raja - Scientific Reports, 2024 - d-nb.info
Compact multi‑rotor unmanned aerial vehicles (UAVs) can be operated in many challenging
environmental conditions. In case the UAV requires certain considerations in designing like …