Security Engineering Project - System Aware Cyber Security for an Autonomous Surveillance System On Board an Unmanned Aerial Vehicle

2014 ◽  
Author(s):  
Barry Horowitz ◽  
Peter Beling ◽  
Kevin Skadron ◽  
Ron D. Williams ◽  
William Melvin
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Cyber Security ◽  
Surveillance System ◽  
Engineering Project ◽  
Security Engineering ◽  
Aerial Vehicle

An Overview of Unmanned Aerial Vehicle: Cyber Security Perspective

2016 ◽  
Author(s):  
Young Sil Lee ◽  
◽  
Young-Jin Kang ◽  
Sang-Gon Lee ◽  
HoonJae Lee ◽  
...  
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Cyber Security ◽  
Aerial Vehicle

scholarly journals Unmanned Aerial Vehicle Design for Application in Cyber Security

2021 ◽  
pp. 151-153
Author(s):  
M. K. Gambaryan
Keyword(s):  
Low Power ◽  
Unmanned Aerial Vehicle ◽  
Cyber Security ◽  
Modular Design ◽  
Cyber Attacks ◽  
Vehicle Design ◽  
Wireless Technology ◽  
Power Devices ◽  
Man In The Middle ◽  
Aerial Vehicle

In this paper a small copter size unmanned aerial Vehicle (UAV) has been designed as a platform for a flying computer station to carry out cyber-attacks (Jamming, Spoofing, Man in the Middle, etc.) on devices that utilize wireless technologies, WiFi in particular. A yagi-patch hybrid antenna designed for 2.4 GHz freely rotates on two axes, thus allowing the drone to perform attacks on low power devices up to ranges of 300 meters. The modular design of the UAV allows for quick swapping of modules depending on the specific wireless technology used by the target device.

Model and Auto Take-Off Control Law Design of Unmanned Aerial Vehicle

2011 ◽  
Vol 383-390 ◽  
pp. 1524-1530
Author(s):  
Hui Song ◽  
Xin Chen
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Rotation Speed ◽  
Aerodynamic Characteristics ◽  
Control Law ◽  
Engineering Project ◽  
Dynamical Characteristics ◽  
Control Scheme ◽  
Aerial Vehicle ◽  
Lift Off ◽  
And Control

The Unmanned Aerial Vehicle (UAV) has special dynamical characteristics in ground motion different from that of flight in the airborne. The forces and moments on the ground to the UAV differ during taxiing, according to the different mechanical and aerodynamic characteristics. An all-states nonlinear model is established by studying on a sample UAV. Rotation speed and lift off speed is determined, finally a control law including longitudinal and lateral control for automatic take-off is designed. Results of simulation show that the model and control scheme can not only join the ground taxiing and flight in the airborne smoothly, but also has a high value in realizing engineering project.

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