RFlySim: Automatic test platform for UAV autopilot systems with FPGA-based hardware-in-the-loop simulations

2021 ◽  
pp. 106727
Author(s):  
Xunhua Dai ◽  
Chenxu Ke ◽  
Quan Quan ◽  
Kai-Yuan Cai
2014 ◽  
Vol 556-562 ◽  
pp. 2567-2570
Author(s):  
He Jia Li ◽  
Xue Wang ◽  
Hai Feng Xu ◽  
Cheng Yao ◽  
Wen Ju Gao ◽  
...  

Aiming the problem of the armored vehicle's gun control system that there are many kinds of internal devices, complex fault reasons ,but no all-around and online fault diagnosis and state inspection mean, The automatic test platform for the gyroscope group with performance test and fault diagnosis for component and circuit is designed .The platform based on dependency matrix and optimal criterion of the maximum failure feature information entropy optimize test points ,choose optimal test points design. Performance test module is created and provides test result information for fault dictionary in fault diagnosis module. Automatic test platform is able to locate the circuit component failure.The platform is tested by actual vehicle experiment, and the results prove the reliability and validity of the platform.


Author(s):  
Hongyu Wang ◽  
Djamaleddine Azaizia ◽  
Cunyue Lu ◽  
Baomin Zhang ◽  
Xun Zhao ◽  
...  

Author(s):  
John Parker ◽  
Christopher Poston ◽  
Richard Roser ◽  
Joel Anstrom ◽  
Timothy Cleary ◽  
...  

This technical paper provides instruction by example on how to apply hardware-in-the-loop (HIL) simulation for accelerated development of a complex control algorithm. The instruction provided in this technical paper is directed to HIL test bench setup, software, simulated and real hardware, and test methods. As an example, the authors reference their collaborative development project of the last couple of years, now completed. The objective of that project was to develop a demand-driven hydrogen production system and integrate it with a hydrogen-fueled internal combustion engine-powered vehicle test platform. The instruction provided in this technical paper is supported by data from the referenced project example.


Sensors ◽  
2020 ◽  
Vol 20 (7) ◽  
pp. 1947
Author(s):  
Diogo de Oliveira Costa ◽  
Neusa Maria Franco Oliveira ◽  
Roberto d’Amore

This article analyzes the use of Remotely Piloted Aircrafts (RPA) in VOR (Very High Frequency Omnidirectional Range) flight inspection. Initially, tests were performed to check whether the Autopilot Positioning System (APS) met the regulatory requirements. The results of these tests indicated that the APS provided information within the standard regulations. A Hardware in the Loop (HIL) platform was implemented to perform flight tests following the waypoints generated by a mission automation routine. One test was performed without introducing disturbance into the proposed test platform. The other four tests were performed introducing errors in latitude and longitude in the APS into the platform. The errors introduced had the same characteristics as those measured in the initial tests, in order for the simulation tests to be as similar as possible to the real situation. The tests performed with positioning errors only did not lead to false misalignment detection. However, introducing positioning errors and a 4° VOR misalignment error, a misalignment of 3.99° was observed during the flight test. This is a value greater than the maximum one allowed by the regulations, and the system indicates the VOR misalignment. Five flight inspection tests were performed. In addition to the APS errors, tests with a modulation error were also conducted. Introducing a 4° VOR misalignment in conjunction with modulation error, a misalignment of 4.02° was observed, resulting in successful misalignment detection.


2018 ◽  
Vol 51 (4) ◽  
pp. 119-124 ◽  
Author(s):  
Muhsin Hancer ◽  
Rahman Bitirgen ◽  
Ismail Bayezit

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