Zobrazeno 1 - 10
of 40
pro vyhledávání: '"Geng, Qingbo"'
Publikováno v:
In IFAC PapersOnLine 2015 48(28):514-519
Akademický článek
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Publikováno v:
IET Control Theory & Applications. 9:944-962
For a class of discrete-time multi-variable systems with time-varying parametric uncertainty, the parameter identification method and switching control architecture are developed in this study to implement smooth switching control. Specifically, the
Publikováno v:
2016 31st Youth Academic Annual Conference of Chinese Association of Automation (YAC).
This paper introduces a flying-wing tail-sitter aircraft which can switch between vertical flight mode (rotary-wing mode) and level flight mode (fixed-wing mode). Equipped with two propellers and two elevons, the aircraft can fly by controlling these
Publikováno v:
2015 34th Chinese Control Conference (CCC).
For Take-off and Landing Controller of Fixed-wing Unmanned Aerial Vehicles (UAV) in the presence of strong disturbances and unknown ground effects, a High Performance L 1 Adaptive Control (HPL 1 AC) method is proposed in this paper. HPL 1 AC is based
Autor:
Kaabche Issam, Geng Qingbo
Publikováno v:
Fifth International Conference on Intelligent Control and Information Processing.
Recently, quadrotors have drawn the attention of many researchers, which is due principally to the broad range of military and civilian purposes [1]. In this paper, three kinds of control strategies (PID, Sliding mode and Backstepping) are adopted to
Publikováno v:
Fifth International Conference on Intelligent Control and Information Processing.
Quad-rotor helicopter is a popular platform for unmanned aerial vehicle (UAV) research due to its simplicity of structure and maintenance as well as the capability of hovering and vertical take-off and landing. The attitude controller is of great imp
Akademický článek
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Publikováno v:
2012 Fifth International Symposium on Computational Intelligence and Design.
The 3-DOF four rotors system is a typical high-order, nonlinear, multi-variable and strong coupling complex system. the motion equations of the yaw, pitch and roll axes can simulate the flight characteristics of the actual helicopter. It is usually d
Publikováno v:
2016 12th IEEE International Conference on Control & Automation (ICCA); 2016, p413-418, 6p