Design of Multi-Input Multi-Output Controller for an Unmanned Aerial Vehicle by Eigenstructure Assignment Method

سال انتشار: 1400
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 131

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شناسه ملی سند علمی:

JR_JASTI-14-1_011

تاریخ نمایه سازی: 8 مرداد 1402

چکیده مقاله:

The purpose of this paper is to present a Multi-Input Multi-Output (MIMO) linear controller based on the eigenstructure assignment method for a fixed-wing Unmanned Aerial Vehicle (UAV) in longitudinal and lateral-directional channels. To this end, a six degree-of-freedom model of the aerial vehicle is considered, where dynamic modes of the system in each channel are analyzed, and the effect of each dynamic mode on state and output variables of the system is investigated. Then, the eigenvalue and eigenvector parameters of the designed controller are appropriately assigned for the system dynamic modes in each channel. In addition, the system requirements of each dynamic mode are satisfied with the proposed controller, and the adverse interaction between the system state variables is minimized. The capability and effectiveness of the designed controller in a desired maneuver are demonstrated with a nonlinear model simulation of a fixed-wing UAV. In this regard, the results in longitudinal and lateral-directional channels are presented.

کلیدواژه ها:

Eigenstructure assignment ، Multi-Input - Multi-Output Controller ، Unmanned Aerial Vehicle

نویسندگان

Ali Motamedi

Amirkabir University of Technology, Department of Aerospace Engineering

Abolghasem Naghash

Amirkabir University of Technology, Department of Aerospace Engineering

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  • L. Faleiro and R. Pratt, "Eigenstructure assignment applied to the ...
  • A. Andry, E. Shapiro, and J. Chung, "Eigenstructure assignment for ...
  • D. Gutiérrez and R. Salazar-Varas, "Using eigenstructure decompositions of time-varying ...
  • M. Serra, F. Resta, and F. Ripamonti, "An active control ...
  • Y. Yuan and H. Liu, "An iterative updating method for ...
  • C. Kazantzidou, T. Perez, and F. Valentinis, "Eigenstructure assignment for ...
  • K. M. Sobel and E. Y. Shapiro, "Application of eigenstructure ...
  • K. M. Sobel and F. J. Lallman, "Eigenstructure assignment for ...
  • O. Albostan and M. Gökaşan, "Mode decoupling robust eigenstructure assignment ...
  • G. ALBOSTAN and M. Gokasan, "High angle of attack manoeuvring ...
  • M. R. Mortazavi and A. Naghash, "Pitch and flight path ...
  • A. R. Mehrabian and J. Roshanian, "Skid-to-turn missile autopilot design ...
  • A. Ashrafi, M. Mortazavi, A. gholami, “Linear control for duct ...
  • H. Noura and F. Bateman, "Control of an Unmanned Aerial ...
  • J. Roskam, Airplane flight dynamics and automatic flight controls. DARcorporation, ...
  • A. Askari, M. Mortazavi, H. Talebi, and A. Motamedi, "A ...
  • A. Motamedi, Mortazavi, j. Roshani yan, Babaii, “Continuous Curvature Trajectory ...
  • H. Nobahari and A. Sharifi, "Multiple model extended continuous ant ...
  • R. W. Beard and T. W. McLain, Small unmanned aircraft. ...
  • U.S. Military Specification, MIL-F-۸۷۸۵C, ۱۹۸۰, http://www.mechanics. iei.liu.se/edu_ug/tmme۵۰/۸۷۸۵c.pdf ...
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