УДК: 629.7.018.2

AN AUTOMATED MEASURING COMPLEX FOR RESEARCH PARAMETERS OF UNMANNED AERIAL VEHICLE

Oleg V. Drozd1, Pavel V. Avlasko2

Abstract. When research, design and development of unmanned aerial vehicles (UAV), a key role belongs to automated measuring complexes for its simulation and prototyping electromechanical system with digital control. The complex is based on the modular measuring platform and also includes a set of various sensitive elements for forces, vibration, speed, torque, video and sound registration. Design and debugging of such system is suggested performs by use model-based approach with automated simulation tools. In the article, the simulation model for research parameters of unmanned aerial vehicles is discussed. This model is suggested to develop based on Gough–Stewart platform (6-axes platform manipulator) with UAV mounted on it. The researched model includes the UAV’s trajectory generator, automatic control device for UAV, kinematic manipulator model and decision subsystem to define the current attitude of the manipulator dynamic side. Also, the presented model can function in conjunction with the user interface of the measuring complex and can be used to evaluate the parameters of complex functioning. The article also describes the procedure for one of the functional assessment stages of the UAV engine test complex, notably, the assessment of the tensometric measurement accuracy.

Keywords: unmanned aerial vehicle, simulation, functional modeling, Gough–Stewart platform, model-based approach

For citation: Drozd O. V., Avlasko P. V. An automated measuring complex for research parameters of unmanned aerial vehicle // Digitalization. 2022, 3 (2), pp. 31—40. [in Russian]. https://doi.org/10.37993/2712-8733-2022-3-2-31-40. EDN: EKDTKR

References

1.       Abdellatif H., Heimann B. Computational efficient inverse dynamics of 6-DOF fully parallel manipulators by using the Lagrangian formalism // Mechanism and Machine Theory. 2009. V. 44. № 1. P. 192-207.  

2.       Chen F., Dong W., Yang M., Sun L., Du Z. A PZT Actuated 6-DOF Positioning System for Space Optics Alignment // IEEE/ASME Transactions on Mechatronics. 2019. V. 24. № 6. P. 2827-2838.           

3.       Cho H., Lee S., Han C. Experimental study on the aerodynamic characteristics of a fighter-type aircraft model in close formation fligh // Journal of Mechanical Science and Technology. 2014. V. 28. № 8. P. 3059-3065.     

4.       Dasgupta B., Mruthyunjaya T. S. A Newton-Euler formulation for the inverse dynamics of the Stewart platform manipulator // Mechanism and Machine Theory. 1998. V. 33. № 8. P. 1135-1152.    

5.       Gallardo J., Alcaraz L. A. Kinematics of the Gough-Stewart Platform by Means of the Newton-homotopy Method // IEEE Latin America Transactions. 2018. V. 16. № 12. P. 2850-2856.

6.       Hamel P. G. (ed.) In-Flight Simulators and Fly-by-Wire/Light Demonstrators. Cham: Springer International Publishing, 2017, 345 p.              

7.       Liu J., Yue Z., Geng X., Wen S., Yan W. Long-Life Design and Test Technology of Typical Aircraft Structures. Singapore: Springer Singapore, 2018, 154 p.             

8.       Liu M., Egan G. K., Santoso F. Modeling, Autopilot Design, and Field Tuning of a UAV With Minimum Control Surfaces // IEEE Transactions on Control Systems Technology. 2015. V. 23. № 6. P. 2353-2360.            

9.       Luces M., Mills J. K., Benhabib B. A Review of Redundant Parallel Kinematic Mechanisms // Journal of Intelligent & Robotic Systems. 2017. V. 86. № 2. P. 175-198.  EDN: YXEOUJ          

10.     Mardiyanto R. Development of Autopilot system of Unmanned Aerial Vehicle for Aerial Mapping Application // International Seminar on Intelligent Technology and Its Applications (ISITIA). 2018. P. 357-361.       

11.     Min-Jie L., Cong-Xin L., Chong-Ni L. Dynamics analysis of the Gough-Stewart platform manipulator // IEEE Transactions on Robotics and Automation. 2000. V. 16. № 1. P. 94-98.         

12.     Ni K., Liu Y., Mei Z., Wu T., Hu Y., Wen H., Wang Y. Electrical and Electronic Technologies in More-Electric Aircraft: A Review // IEEE Access. 2019. V. 7. P. 76145-76166.

13.     Paw Y. C., Balas G. J. Development and application of an integrated framework for small UAV flight control development // Mechatronics. 2011. V. 21. № 5. P. 789-802.  EDN: JYJBJR    

14.     Pradipta J., Sawodny O. ServoFlight: pneumatically actuated full flight simulator /// International Journal of Fluid Power. 2016. V. 17. № 1. P. 49-64.  EDN: YWOUAT       

15.     Romano F., Sorrentino A., Pellone L., Mercurio U., Notarnicola L. New design paradigms and approaches for aircraft composite structures // Multiscale and Multidisciplinary Modeling, Experiments and Design. 2019. V. 2. № 2. P. 75-87.         

16.     Ruiz-Tolosa J. R., Castillo E. From Vectors to Tensors. Berlin Heidelberg: Springer-Verlag, 2005, 670 p.  

17.     Sedda S., Sardu C., Iuso G. Investigation of a novel VTOL aircraft concept for operations in urban areas // Aerotecnica Missili & Spazio. 2017. V. 96. № 3. P. 165-175.            

18.     Shukla A., Karki H., Behera L., Jamshidi M. M. Teleoperation by Using Nonisomorphic Mechanisms in the Master-Slave Configuration for Speed Control // IEEE Systems Journal. 2018. V. 12. № 2. P. 1369-1380.            

19.     Stewart D. A Platform with Six Degrees of Freedom // Proceedings of the Institution of Mechanical Engineers. 1965. V. 180. № 1. P. 371-386.    

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