UAS Flight Simulation with Hardware-in-the-loop Testing and Vision Generation

Author(s):  
Jeffery Saunders ◽  
Randal Beard
2018 ◽  
Vol 90 (9) ◽  
pp. 1428-1437 ◽  
Author(s):  
Irum Inayat ◽  
Rooh ul Amin ◽  
Malik Mazhar Ali

Purpose This paper aims to propose an improved and computationally efficient motion simulation of a flexible variable sweep aircraft. Design/methodology/approach The motion simulation is performed on hardware-in-the-loop simulation setup using 6 degree-of-freedom motion platform. The dynamic model of a flexible variable sweep aircraft, Rockwell B-1 Lancer is presented using equations of motions for combined rigid and flexible motions. The peak filter is introduced as a new method to separate flexible motion from aircraft motion data. Standard adaptive washout filter is modified and redesigned for an accurate flexible aircraft flight simulation. The flight data are generated using FlightGear software. Another motion profile with significant oscillations is also tested. The peak filter and the modified adaptive washout filter both are used to process the data according to the motion envelop of motion platform. Findings The performance of the modified adaptive washout filter is evaluated using hardware-in-the-loop simulation setup and results are compared with the standard adaptive washout filter. Results exhibit that the proposed method is computationally cost-effective and improves the motion simulation of flexible aircraft with close to realistic motion cues. Originality/value The proposed work presents motion simulation of a flexible aircraft by introducing a peak filter to extract flexible motion in contrast to the traditional motion separation methods. Also, a modified adaptive washout filter is designed and implemented in place of the traditional washout filters for improved flexible aircraft flight motion simulation.


2015 ◽  
Vol 789-790 ◽  
pp. 681-687 ◽  
Author(s):  
Emre Atlas ◽  
Melike Irem Erdoğan ◽  
Onur Baki Ertin ◽  
Anıl Güçlü ◽  
Yusuf Eren Saygi ◽  
...  

A hardware-in-the-loop (HIL) platform for unmanned air vehicle (UAV) systems is designed that demonstrates flight attitudes on yaw, pitch and roll axes. The design combines a sophisticated flight simulation software with a platform capable of moving 360 degrees on all axes. This enables the testing of the flight sensors and autopilot algorithms for all sorts of scenarios including emergency and acrobatic cases where an indefinite number of full rotations in the yaw, roll and pitch might take place.


2010 ◽  
Vol 130 (5) ◽  
pp. 646-654 ◽  
Author(s):  
Miao Hong ◽  
Satoshi Horie ◽  
Yushi Miura ◽  
Tosifumi Ise ◽  
Yuki Sato ◽  
...  

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