Cover Image

ADAPTIVE CONTROLER OF MAJOR FUNCTION FOR CONTROLLING ELASTIC AERIAL VEHICLE

Thanh Duc Nguyen, Phuong Viet Nguyen

Abstract


An adaptive controller of the major function for an aerial vehicle's (AV) longitudinal motion with account for the wing aeroelasticity is discussed in this research. A nonlinear mathematical model of resilient aircraft's longitudinal motion is designed. Adaptive control system of a resilient AV is built by means of majorizing function and its efficiency is tested under the uncertainty parameter function of AV model.

Full Text:

Pdf

References


Tewari A. “Aeroservoelasticity Modeling and Control”// New York: Springer. 2015.

T. Theodorsen. “General Theory of Aerodynamic Instability and the Mechanism of Flutter” // NACA Report 496 (1935).

Путов В.В., Шелудько В.Н. “Адаптивные и модальные системы объектами”// СПб.: Элмор, 2007 - 243 с.

A. Lebedev, L. Cherubrovkin. “Flight Dynamics of Unmanned Aerial Vehicles”. Moscow, 1962. 487 pages.

V. Putov. “Direct and indirect searchless adaptive systems with majorizing functions and their application to the control of nonlinear resilient mechanical objects”// Publishing House Novie Tehnologii - Mechatronics, automation and control - Issue #10 - 2007 - pp. 4-11

V. Putov. “Comparative Research of Adaptive Systems on Condition and Output in Control of Unmanned Aerial Vehicle/ V. Putov // Izvestia 'LETI'. 2016. Issue # 6. pp. 41 -44.


Refbacks



Indexed by: Google Scholar.

Lớp dạy vẽ ở Mỹ Đình