scholarly journals Solid State Sensors - Practical Implementation in Unmanned Aerial Vehicles (UAVs)

2012 ◽  
Vol 47 ◽  
pp. 1386-1389 ◽  
Author(s):  
Piotr J. Dziuban ◽  
Anna Wojnar ◽  
Artur Zolich ◽  
Krzysztof Cisek ◽  
Wojciech Szumiński
Keyword(s):  
Solid State ◽  
Unmanned Aerial Vehicles ◽  
Practical Implementation ◽  
Aerial Vehicles

A method for autonomous collision-free navigation of a quadrotor UAV in unknown tunnel-like environments

Robotica ◽  
2021 ◽  
pp. 1-27
Author(s):  
Taha Elmokadem ◽  
Andrey V. Savkin
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Autonomous Underwater Vehicles ◽  
Three Dimensional ◽  
Underwater Vehicles ◽  
Practical Implementation ◽  
Challenging Problem ◽  
Quadrotor Uav ◽  
Navigation Algorithm ◽  
Aerial Vehicles ◽  
Quadrotor Uavs

Abstract Unmanned aerial vehicles (UAVs) have become essential tools for exploring, mapping and inspection of unknown three-dimensional (3D) tunnel-like environments which is a very challenging problem. A computationally light navigation algorithm is developed in this paper for quadrotor UAVs to autonomously guide the vehicle through such environments. It uses sensors observations to safely guide the UAV along the tunnel axis while avoiding collisions with its walls. The approach is evaluated using several computer simulations with realistic sensing models and practical implementation with a quadrotor UAV. The proposed method is also applicable to other UAV types and autonomous underwater vehicles.

scholarly journals Simulation of platform-free inertial navigation system of unmanned aerial vehicles based on neural network algorithms

2021 ◽  
Vol 1 (2(57)) ◽  
pp. 15-19
Author(s):  
Robert Bieliakov
Keyword(s):  
Neural Network ◽  
Unmanned Aerial Vehicles ◽  
Adaptive Learning ◽  
Microelectromechanical Systems ◽  
Inertial Navigation ◽  
Process Time ◽  
Practical Implementation ◽  
Network Algorithms ◽  
Navigation Data ◽  
Aerial Vehicles

The object of research is the process of controlling the trajectory of unmanned aerial vehicles (UAVs) in autonomous flight mode based on neural network algorithms. The study is based on the application of numerical-analytical approach to the selection of modern technical solutions for the construction of standard models of platformless inertial navigation systems (BINS) for micro and small UAVs, followed by support for assumptions. The results of simulation in the Matlab environment allowed to simulate the operation of the UAV control system based on MEMS technology (using microelectromechanical systems) and Arduino microcomputers. It was also possible to experimentally determine the nature of the influence of the structure of the selected neural network on the process of formation of navigation data during the disappearance of the GPS signal. Thus, to evaluate the effectiveness of the proposed solutions for the construction of BINS, a comparative analysis of the application of two algorithms ELM (Extreme Learning Machine)-Kalman and WANN (Wavelet Artificial Neural Network)-RNN (Recurrent Neural Network)-Madgwick in the form of two experiments. The purpose of the experiments was to determine: the study of the influence of the number of neurons of the latent level of the neural network on the accuracy of approximation of navigation data; determining the speed of the process of adaptive learning of neural network algorithms BINS UAV. The results of the experiments showed that the application of the algorithm based on ELM-Kalman provides better accuracy of learning the BINS neural network compared to the WANN-RNN-Madgwick algorithm. However, it should be noted that the accuracy of learning improved with the number of neurons in the structure of the latent level <500, which iincreases computational complexity and increases the learning process time. This can complicate the practical implementation using micro- and small UAV equipment. In addition, thanks to the simulation, the result of the study of the application of the proposed neural network algorithms to replace the input data instead of GPS signals to the input BINS, allowed to estimate the positioning error during the disappearance of GPS signals. Also, the application of the WANN-RNN-Madgwick algorithm allows to approximate and extrapolate the input signals of navigation parameters in a dynamic environment, while the process of adaptive learning in real time.

scholarly journals Design and Dynamics of Kinetic Launcher for Unmanned Aerial Vehicles

2020 ◽  
Vol 10 (8) ◽  
pp. 2949
Author(s):  
Mirosław Kondratiuk ◽  
Leszek Ambroziak
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Electrical Energy ◽  
Practical Implementation ◽  
The Novel ◽  
Electromagnetic Launchers ◽  
Aerial Vehicles ◽  
Start Up ◽  
Motion Characteristics ◽  
Novel Concept ◽  
Operator Safety

Assisting in the starting procedure of Unmanned Aerial Vehicles (UAVs) is one of many very important areas of modern aviation research. Supported start-up saves fuel or electrical energy, increases operator safety and level of autonomy, extends the application area, and, in some applications, even enables the operator to shape the motion characteristics of the initial phase of a UAV’s flight. Currently used solutions, depending on an aircraft’s class, are based on the utilization of rubber, pneumatic or electromagnetic launchers. All of these launchers are used for the medium class of UAVs and all of them use the potential energy previously stored in stretched rubber, compressed air or electrical voltage. In this paper, authors propose the novel concept of a launcher powered through kinetic energy stored in a rotary wheel driven by an electric motor. Using the transmission systems of the drive and the controlled clutch and an electromagnetic brake, it is possible to precisely control the speed and acceleration of the launched object. Within the paper, the authors present and discuss the applied equations of dynamics, the results of a simulation that was carried out using the MATLAB/Simulink software and a conceptual CAD model of preliminary engineering solutions for the kinetic UAV launcher. The work is summarized in the conclusions section, which details the practical implementation of the device.

scholarly journals Simulation of quadcopter flight altitude stabilization system

2020 ◽  
Vol 33 (02) ◽  
pp. 638-650
Author(s):  
Mikhail Yu. Babich ◽  
Mikhail M. Butaev ◽  
Dmitry V. Pashchenko ◽  
Alexey I. Martyshkin ◽  
Dmitry A. Trokoz
Keyword(s):  
Mathematical Model ◽  
Unmanned Aerial Vehicles ◽  
Control Algorithm ◽  
Angular Position ◽  
The Other ◽  
Practical Implementation ◽  
Stabilization System ◽  
Flight Altitude ◽  
Aerial Vehicles ◽  
Aerial Vehicle

Recently, unmanned aerial vehicles have been an important part of scientific research in various fields. Quadrocopter is an unmanned aerial vehicle with four rotors, two of which rotate clockwise, the other two counterclockwise. Changing the speed of screw rotation allows you to control the movement of the apparatus. The article proposed and tested a mathematical model of a quadcopter. They presented the development of a simple control algorithm that allows to stabilize the height and angular position. The research results show the efficiency of the algorithm and the possibility of its practical implementation. The developed mathematical model can be used instead of a real quadcopter, which will significantly reduce the time during research, as well as avoid the quadrocopter damage, reducing the number of launches.

scholarly journals Practical Aspects of Design and Testing Unmanned Aerial Vehicles

2020 ◽  
Vol 14 (1) ◽  
pp. 50-58
Author(s):  
Patryk Szywalski ◽  
Andrzej Waindok
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Global Positioning System ◽  
Practical Implementation ◽  
Positioning System ◽  
Positioning Systems ◽  
Autonomous Flight ◽  
Aerial Vehicles ◽  
Global Positioning ◽  
Aerial Vehicle ◽  
Design And Testing

AbstractA design of an unmanned aerial vehicle (UAV) construction, intended for autonomous flights in a group, was presented in this article. The design assumptions, practical implementation and results of the experiments were given. Some of the frame parts were made using 3D printing technology. It not only reduces the costs but also allows for better fitting of the covers to the electronics, which additionally protects them against shocks and dirt. The most difficult task was to develop the proper navigation system. Owing to high costs of precision positioning systems, common global positioning system (GPS) receivers were used. Their disadvantage is the floating position error. The original software was also described. It controls the device, allows performing autonomous flight along a pre-determined route, analyses all parameters of the drone and sends them in a real time to the operator. The tests of the system were carried out and presented in the article, as well.

A Piezocomposite Actuated Propeller With an Onboard Power Generator

2020 ◽  
Author(s):  
Bharg Shah ◽  
Onur Bilgen
Keyword(s):  
Solid State ◽  
Unmanned Aerial Vehicles ◽  
Rotor Blade ◽  
Mechanical Energy ◽  
Electrical Energy ◽  
Power Generator ◽  
Single Degree ◽  
Model Scale ◽  
Aerial Vehicles ◽  
Electromagnetic Power

Abstract This paper presents an application of a novel piezocomposite rotor system on a model-scale helicopter. The piezocomposite rotor concept can be implemented on various rotary systems, including small unmanned aerial vehicles, and tandem rotor, multi-rotor, single-rotor and other rotary systems. Based on authors’ previous research, a new design of the so-called solid-state rotor concept is implemented on a single degree of the freedom apparatus that the derived from the model-scale helicopter. An electromagnetic power generator is used to convert the mechanical energy due to the rotation of the generator into electrical energy, and this is used to actuate the piezocomposite blades. The actuation by the piezocomposite actuators on the rotor blade results in a change of the camber of the rotor blade. The change in camber generates an increase of thrust.

scholarly journals Aspects of Equipping Transport Facilities with Systems for Controlling Routes of Unmanned Aerial Vehicles

2021 ◽  
Vol 18 (4) ◽  
pp. 84-96
Author(s):  
S. V. Shvetsova
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Emergency Situation ◽  
Transport Infrastructure ◽  
Practical Implementation ◽  
Technical Equipment ◽  
Ground Vehicles ◽  
Routing Problem ◽  
Scientific Methods ◽  
Aerial Vehicles ◽  
Analysis And Synthesis

Currently, the problem of ensuring safety of flights of unmanned aerial vehicles (UAVs) over the territory of transport infrastructure facilities (TIF), primarily airports, remains topical.In one of the previous works, the author together with the co-author proposed a method for increasing safety of movement of unmanned aerial vehicles and the system for controlling the routes of unmanned aerial vehicles (hereinafter – route control system, RCS) that implements it, which makes it possible to improve safety and security of UAV traffic at transport infrastructure facilities by limiting UAV traffic area strictly to a dedicated air corridor (DAC). The development of this system creates the prerequisites for removing the existing restrictions on the use of unmanned aerial vehicles at transport infrastructure facilities.For practical implementation of the proposed system, it is relevant to develop a method of placing RCS at transport infrastructure facilities. This condition can be justified by the fact that RCS, as a rule, will be located under conditions of dense infrastructural development, including dangerous technical elements of technical equipment, a collision of a UAV with which can lead to an emergency situation (ES); besides, the movement of air/ground vehicles will be carried out in the immediate vicinity of RCS along transport routes/corridors, and employees, passengers and visitors of TIF will move along the pedestrian paths.The objective of this study – to develop a methodology for placing systems controlling routes of unmanned aerial vehicles at transport infrastructure facilities.The study conducted with well-known scientific methods, including the basic routing problem posed by Dantzig and Ramser, modelling, analysis, and synthesis, made it possible to develop a method for placing RCS for unmanned aerial vehicles at transport infrastructure facilities. The practical application of the proposed methodology makes it possible to build routes for movement of UAV at TIF, to form a network of dedicated air corridors for UAV at TIF operated in relationship with the system, determine the optimal location of the RCS elements at TIF.

Development of thickened semi-synthetic engine oil M-5z / 20 AERO for four-stroke gasoline engines aircraft piston of unmanned aerial vehicles (UAVs)

2020 ◽  
Vol 06 ◽  
pp. 44-47
Author(s):  
A.A. Moykin ◽  
◽  
A.S. Medzhibovsky ◽  
S.A. Kriushin ◽  
M.V. Seleznev ◽  
...  
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Engine Oil ◽  
Motor Oil ◽  
Gasoline Engines ◽  
State Research Institute ◽  
Technical Requirements ◽  
Aerial Vehicles ◽  
State Research ◽  
Industrial Batch ◽  
The Russian Federation

Nowadays, the creation of remotely-piloted aerial vehicles for various purposes is regarded as one of the most relevant and promising trends of aircraft development. FAU "25 State Research Institute of Chemmotology of the Ministry of Defense of the Russian Federation" have studied the operation features of aircraft piston engines and developed technical requirements for motor oil for piston four-stroke UAV engines, as well as a new engine oil M-5z/20 AERO in cooperation with NPP KVALITET, LLC. Based on the complex of qualification tests, the stated operational properties of the experimental-industrial batch of M-5z/20 AERO oil are generally confirmed.

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