scholarly journals Research on Digital Remote Control Technology of Surveying and Unmanned Aerial Vehicle

2018 ◽  
Author(s):  
Na Zhang
Keyword(s):  
Remote Control ◽  
Unmanned Aerial Vehicle ◽  
Control Technology ◽  
Aerial Vehicle

scholarly journals Drone in NBC disaster

2018 ◽  
Vol 5 (12) ◽  
pp. 5476
Author(s):  
Yong Han Kim
Keyword(s):  
Remote Control ◽  
Unmanned Aerial Vehicle ◽  
Human Exposure ◽  
Nerve Agent ◽  
Remote Laboratory ◽  
Disaster Area ◽  
Rescue Team ◽  
Aerial Vehicle ◽  
Rescue Personnel

Nuclear, Biological and chemical disasters are tragic and should never happen. Unavoidably occurred, access and reach are difficult because rescue personnel are exposed to hazards. Drone is an unmanned aerial vehicle that can be operated by remote control or autonomous aviation. It has some advantages in NBC disaster as followings:First, drone can take a picture and record the scene in contaminated zone. Communication with injured is also possible without exposure to rescue team. Triage can be performed by analysis of movement, breathing and responsiveness, etc.Second, atropine and oxime are essential to nerve agent poisoning. It can be delivered by drone only inside contaminated zone for survivors.Third, drone can collect specimen without human exposure. Investigator can analyze the extent of pollution in remote laboratory with this specimen.Fourth, survivor can be evacuated from disaster area by drone itself. This operation needs heavy capability that would lift patients.I hope that NBC disaster could be overcome with this useful modern convenience.

Roll aerodynamic characteristics study of an unmanned aerial vehicle based on circulation control technology

2017 ◽  
Vol 233 (3) ◽  
pp. 871-882
Author(s):  
Kun Chen ◽  
Zhiwei Shi ◽  
Jiachen Zhu ◽  
Haiyang Wang ◽  
Junquan Fu
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Flight Control ◽  
Attitude Control ◽  
Aerodynamic Force ◽  
Flight Test ◽  
Scale Model ◽  
Maximum Efficiency ◽  
Control Technology ◽  
Circulation Control ◽  
Aerial Vehicle

To explore the control efficiency of circulation flow control technology, a circulation control actuator with an independent gas source has been designed and applied in roll attitude control of a small unmanned aerial vehicle. The circulation control devices are arranged at the two ends of the wing on an unmanned aerial vehicle scale model, the changes in aerodynamic force and aerodynamic moment caused by turning on the actuator are measured in a wind tunnel, and the flow field characteristics are analysed using particle image velocimetry technology. The flight control effect of the roll attitude is verified via a flight test. Experimental and flight test results show that the control of roll attitude can be achieved by turning on the circulation control actuator on one side, and the maximum efficiency that the circulation control generates is equivalent to 8° aileron deflection with production of a favorable yaw moment to achieve a coordinated turn. The circulation control actuator can increase lift and reduce drag when opened on both sides simultaneously. The maximum lift-to-drag ratio of the UAV increased from 5 to 9, and this approach can also suppress flow separation and delay stall at high angles of attack. The aileron or trailing edge flaps can be replaced with circulation control actuators, and the circulation control technology can also be applied to aerodynamic performance improvement and flight control in other types of aircraft.

scholarly journals The IMPLEMENTATION OF AUTONOMOUS WAYPOINT IN RECONNAISSANCE PLANE (UNMANNED AERIAL VEHICLE) UAV GALAK-24 USE WITH MISSION PLANNER

2021 ◽  
Vol 2 (Oktober) ◽  
pp. 47-55
Author(s):  
Luthfan Herlambang ◽  
Eko Kuncoro ◽  
Muhamat Maariful Huda
Keyword(s):  
Remote Control ◽  
Unmanned Aerial Vehicle ◽  
Flight Data ◽  
Air Vehicle ◽  
Aerial Vehicle ◽  
The Military

Abstract: UAV or unmanned aerial vehicle is an air vehicle or what we often call an airplane that is controlled without a crew but controlled by a pilot remotely using a remote control. This study uses quantitative experiment methods because in this study it must be carried out when the UAV is flying using the autonomous waypoint method. Running the UAV with the autonomous waypoint method, we can use the Mission Planner software. First, we have to install the application on the mission planner and install pixhawk on the UAV which will act as the UAV brain that will receive and execute flight commands that will be sent by the mission planner later. The mission planner can also directly display flight data such as UAV altitude, UAV speed, UAV location, then the mission planner can also store flight data run by the UAV. The Autonomous waypoint method has been widely used in the military field, such as to carry out attacks on the enemy, reconnaissance, and patrol in an area quickly, and can also reduce casualties during combat operations.

THE HYDRO PLANING SIMULATION OF FLYING BOAT REMOTE CONTROL MODEL

2016 ◽  
Vol 78 (6) ◽  
Author(s):  
S. Syamsuar ◽  
E. B. Djatmiko ◽  
Erwandi Erwandi ◽  
A. S. Mujahid ◽  
Subchan Subchan
Keyword(s):  
Remote Control ◽  
Unmanned Aerial Vehicle ◽  
Weight Ratio ◽  
Performance Testing ◽  
Control Model ◽  
Three Dimensions ◽  
Pressure Distributions ◽  
Angle Data ◽  
Testing Data ◽  
Aerial Vehicle

The measurement of unknown model to get the three dimensions of object configuration is by using the laser camera photo tracking. The three dimensions model became from solid drawing on the CATIA software. The CFX ANSYS computational fluid dynamics software is used on the 3D of Flying Boat remote control model full configuration. The rectangular and dihedral configurations of the model have Z forces value during acceleration on the water surface. The pressure distributions hydro planing have a good result also. The speeds on the simulation model are around (0 - 25) knots and Angle of Attack, α = 00.  The downwash effect and vortex could be shown in the CFD results. To verify the simulation data analysis is uses the takeoff flight performance testing data during takeoff of Unmanned Aerial Vehicle “Alap alap” with the same Thrust per Weight ratio around 0.4, such as altitude height, airspeed, Z acceleration and pitch angle data. The hump drag of Flying Boat remote control model and the friction during takeoff of Unmanned Aerial Vehicle have been ignored.

scholarly journals System for Effective Remote Control and Monitoring of Radiation Situation Based on Unmanned Aerial Vehicle

2017 ◽  
Vol 13 (4) ◽  
pp. 46-53 ◽  
Author(s):  
Yu.L. Zabulonov ◽  
◽  
V.M. Burtnyak ◽  
L.A. Odukalets ◽  
◽  
...  
Keyword(s):  
Remote Control ◽  
Unmanned Aerial Vehicle ◽  
Aerial Vehicle

The Unmanned Aerial Vehicle Vector Tracking System

2013 ◽  
Vol 401-403 ◽  
pp. 1728-1733
Author(s):  
San Min Shen ◽  
Jing Cui ◽  
Wen Yi Liu
Keyword(s):  
Remote Control ◽  
Unmanned Aerial Vehicle ◽  
High Speed ◽  
Tracking System ◽  
Host Computer ◽  
Single Chip ◽  
Usb Interface ◽  
Vector Tracking ◽  
Aerial Vehicle ◽  
Accurate Position

In the environment of harsh weather or obstacles, the corresponding monitoring department can't achieve remote control and acquire the accurate location of the unmanned aerial vehicle (UAV). According to the existing problem this paper designs a logical control module based on single chip microcomputer (SCM) C8051F040 and UAV real-time tracking system which is positioned by GPS. In this design, through the analysis and extraction of the GPS data, then transmit these data to the host computer through the USB interface with high speed, the unmanned aerial vehicle (UAV) flight vector position such as longitude and altitude information will be displayed by the host computer. After tested for several times, this vector pursuit system can acquire the accurate position of the unmanned aerial vehicle (UAV) and the corresponding flight path within 20 km. To some extent, it provides an effective guarantee for the remote control and monitoring department.

scholarly journals System for Effective Remote Control and Monitoring of Radiation Situation Based on Unmanned Aerial Vehicle

2017 ◽  
Vol 13 (4) ◽  
pp. 40-45 ◽  
Author(s):  
Yu.L. Zabulonov ◽  
◽  
V.M. Burtnyak ◽  
L.A. Odukalets ◽  
◽  
...  
Keyword(s):  
Remote Control ◽  
Unmanned Aerial Vehicle ◽  
Aerial Vehicle
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