scholarly journals The Development of a Hardware-in-the-Loop Simulation System for Unmanned Aerial Vehicle Autopilot Design Using LabVIEW

10.5772/23272 ◽  
2011 ◽  
Author(s):  
Yun-Ping Sun
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Simulation System ◽  
Hardware In The Loop ◽  
Aerial Vehicle

scholarly journals Development of Mobile Ground Control System and GPS Base Auto Tracking Antenna

2018 ◽  
Vol 16 (1) ◽  
pp. 83 ◽  
Author(s):  
Herma Yudhi Irwanto
Keyword(s):  
Control System ◽  
Monitoring System ◽  
Unmanned Aerial Vehicle ◽  
High Speed ◽  
Flight Test ◽  
Simulation System ◽  
Ground Control ◽  
Hardware In The Loop ◽  
Automatic Tracking ◽  
Aerial Vehicle

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

scholarly journals SENSOR FUSION MENGGUNAKAN ACCELEROMETER RATE GYRO (ARG) UNTUK ESTIMASI SUDUT EULER PADA WAHANA TERBANG

ROTASI ◽  
2015 ◽  
Vol 17 (2) ◽  
pp. 84
Author(s):  
Mochammad Ariyanto
Keyword(s):  
Steady State ◽  
Sensor Fusion ◽  
Unmanned Aerial Vehicle ◽  
Hardware In The Loop ◽  
Matlab Simulink ◽  
Rate Gyro ◽  
Aerial Vehicle

Pada sistem control wahana terbang tanpa awak (Unmanned Aerial Vehicle) gabungan sensor accelerometer dan gyroscope sering dipakai untuk mengestimasi sudut Euler seperti sudut roll, pitch, dan yaw. Dalam penelitian ini, akan didesain sebuah instrumen yang dapat digunakan untuk mengestimasi sudut Euler wahana terbang tanpa awak dengan menggunakan gabungan sensor accelerometer dan gyroscope yang menggunakan algoritme sensor fusion seperti Accelerometer Rate Gyro (ARG). Intrumen ini dapat mengukur dan mengestimasi kecepatan sudut putar, percepatan linear, serta sudut Euler wahana terbang tanpa awak. Pada estimasi sudut menggunakan sensor accelerometer, hasilnya akan cukup bagus jika sensor accalerometer dalam kondisi statis, namun jika dalam kondisi dinamik maka sensor accelerometer akan gagal untuk mengestimasi sudut karena berasal dari error ketika mengalami percepatan. Sedangkan jika menggunakan gyroscope, estimasi sudut akan bagus dalam kondisi dinamik, dan buruk jika dalam kondisi statik karena adanya error drift. Oleh karena itu perlu dilakukan sensor fusion antara accelerometer dan gyroscope. Pemodelan dan algoritme sensor fusion dilakukan dalam lingkungan MATLAB/Simulink, implementasinya dilakukan menggunakan hardware in the loop simulation. Evaluasi kinerja sensor fusion yang sudah dibuat akan dilakukan dengan menganalisa pada kondisi steady state. Dari hasil pengujian HILS didapatkan bahwa masih terdapat noise yang relatif kecil pada sudut Euler.

Model-Based Design of UAV Autopilot Software

2013 ◽  
Vol 756-759 ◽  
pp. 2115-2119
Author(s):  
Ming Zuo ◽  
Ying Liu ◽  
Yi Qian ◽  
Xiong Wen Hu ◽  
Xiao Chuan Zhao ◽  
...  
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Field Trials ◽  
Hardware In The Loop ◽  
Control Logic ◽  
Model Based ◽  
Aerial Vehicle ◽  
Trial Cost

This paper presents a Model-Based approach to develop UAV (Unmanned Aerial Vehicle) autopilot software. It employs Simulink to design the flight controller, Stateflow to implement control logic and Matlab coder to automatically generate embedded C code from the model developed. Software in the loop (SIL) and hardware in the loop (HIL) simulations are performed in the laboratory to validate the software developed. Flight trial cost and risks are minimized and the design cycles are greatly shortened. The feasibility and the effectiveness of the approach are verified through results from lab simulations and field trials.

Simulation system of telemetering and telecontrol for unmanned aerial vehicle

2006 ◽  
Vol 21 (9) ◽  
pp. 3-5 ◽  
Author(s):  
Ding Wang ◽  
Jiadong Xu ◽  
Rugui Yao ◽  
Ruifeng Miao
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Simulation System ◽  
Aerial Vehicle

Discuss of Unmanned Plane Braking Experiment Base on Eddy Current Technology

2013 ◽  
Vol 717 ◽  
pp. 333-337
Author(s):  
Wei Chen ◽  
Cheng Zhi Su ◽  
Xu Zhang ◽  
Yue Feng Song
Keyword(s):  
Magnetic Field ◽  
Unmanned Aerial Vehicle ◽  
Eddy Current ◽  
Simulation System ◽  
Test Results ◽  
Current Technology ◽  
Braking System ◽  
Braking Torque ◽  
Aerial Vehicle

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.

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