Unmanned Aerial Vehicle Digital Visual Simulation System Load and Missile Modules Simulation Software Design

Author(s):  
Guoqing Shi ◽  
Xiaoguang Gao
2006 ◽  
Vol 21 (9) ◽  
pp. 3-5 ◽  
Author(s):  
Ding Wang ◽  
Jiadong Xu ◽  
Rugui Yao ◽  
Ruifeng Miao

2013 ◽  
Vol 717 ◽  
pp. 333-337
Author(s):  
Wei Chen ◽  
Cheng Zhi Su ◽  
Xu Zhang ◽  
Yue Feng Song

In the process of unmanned aerial vehicle (uav) landing safely and quickly brake problem,Puts forward a uav electric eddy current braking method.The method through the eddy current and magnetic field interact to produce braking torque. According to the uav braking requirements, Design the uav electric eddy current brake simulation system. Test results show that: Based on the eddy current brake technology the average braking torque for 870N·m is greater than the “inner” type uav brake the average braking torque for 530N·m, Can meet the requirements of the uav braking system, So will the eddy current brake applied to unmanned aerial vehicle is feasible.


2011 ◽  
Vol 181-182 ◽  
pp. 604-609
Author(s):  
Wei Wan ◽  
Yong Hong Hu ◽  
Peng Wu

For accessing data from different channel in UAV (unmanned aerial vehicle) immediately, a method for massive data and multichannel recorder system is introduced. The system hardware composition and functions are described in details. The software design of receiving program is given, including extended UART ports’ initialization and design of interruption scheme. And experiment result shows that the recorder not only record data from UAV successfully but also improve the way to hand the UAV data.


2011 ◽  
Vol 317-319 ◽  
pp. 667-671
Author(s):  
Chuan Chuan Hao ◽  
Zhou Fang ◽  
Ping Li ◽  
Bo Liu

Hardware-in-loop simulation (HILS) is an important approach to the development of Unmanned Aerial Vehicle (UAV) systems. In this paper, a complete HILS system for UAV was constructed based on the dSPACE real-time simulator. To simulate the real world situation, problems such as the GPS signal and accelerometer signal imitation were addressed in the dSPACE framework. The HILS simulation of a UAV’s take-off process was exhibited with comparison to the digital simulation; the results show effectiveness of the proposed HILS system.


2018 ◽  
Vol 16 (1) ◽  
pp. 83 ◽  
Author(s):  
Herma Yudhi Irwanto

Flight test of both rocket and high speed Unmanned Aerial Vehicle (UAV), which is currently developed by LAPAN, can not be separated from the need for a monitoring system of all the attitude of the vehicles. Utilizing and combining some of the available equipment components into a ground control system (GCS) equipped with GPS based auto tracking antenna, makes it easy in previous flight test activities that only do tracking antenna manually. This ground control system is equipped with automatic tracking antenna that always leads to the vehicle, so that the data attitude of flying the vehicle will be maximally monitored and analyzed directly with ease. This system has been tested on a laboratory scale related to testing using hardware in the loop simulation system


2020 ◽  
Vol 20 (4) ◽  
pp. 332-342
Author(s):  
Hyung Jun Park ◽  
Seong Hee Cho ◽  
Kyung-Hwan Jang ◽  
Jin-Woon Seol ◽  
Byung-Gi Kwon ◽  
...  

2018 ◽  
pp. 7-13
Author(s):  
Anton M. Mishchenko ◽  
Sergei S. Rachkovsky ◽  
Vladimir A. Smolin ◽  
Igor V . Yakimenko

Results of experimental studying radiation spatial structure of atmosphere background nonuniformities and of an unmanned aerial vehicle being the detection object are presented. The question on a possibility of its detection using optoelectronic systems against the background of a cloudy field in the near IR wavelength range is also considered.


Author(s):  
Amir Birjandi ◽  
◽  
Valentin Guerry ◽  
Eric Bibeau ◽  
Hamidreza Bolandhemmat ◽  
...  

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