AbstractSince Small Unmanned Helicopter flight attitude control process has strong time- varying characteristics, and there are random disturbances, the conventional control methods with unchanged parameters are often unworkable. An on-line adaptive ADRC control system is designed in this paper. An on-line adaptive ADRC system implements a simultaneous on-line tuning of ADRC rules. The flight experiment showed that the proposed adaptive ADRC system provides quicker response, smaller overshoot, higher precision, robustness and adaptive ability. It satisfies the needs of autonomous flight
In this paper we present a system for automatic control of a quadrocopter based on the adaptive cont...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
This paper presents an actuator dynamics augmentation of the classical Disturbance Observer Based Co...
AbstractSince Small Unmanned Helicopter flight attitude control process has strong time- varying cha...
This article presents design and optimization results from an implementation of a novel disturbance ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2010.This e...
The compound unmanned aircraft is provided with three primary flight modes, which are helicopter fli...
The main purpose of this paper is to develop an onboard adaptive and robust flight control system th...
Published in Journal of Guidance Control and Dynamics, Vol. 28, No. 3, May–June 2005.Presented as P...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2001.Includ...
As the demand for Unmanned Aerial System (UAS) technology increases, the current guidance, navigatio...
Copyright © 2002 by the author(s). Published by the American Institute of Aeronautics and Astronauti...
The article of record as published may be located at http://dx.doi.org/10.2514/1.42056The paper pres...
With the increasing demand for unmanned aerial vehicles (UAVs) in both military and civilian applica...
The method of implementing an adaptive PID controller using a reference model of an unmanned aerial ...
In this paper we present a system for automatic control of a quadrocopter based on the adaptive cont...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
This paper presents an actuator dynamics augmentation of the classical Disturbance Observer Based Co...
AbstractSince Small Unmanned Helicopter flight attitude control process has strong time- varying cha...
This article presents design and optimization results from an implementation of a novel disturbance ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2010.This e...
The compound unmanned aircraft is provided with three primary flight modes, which are helicopter fli...
The main purpose of this paper is to develop an onboard adaptive and robust flight control system th...
Published in Journal of Guidance Control and Dynamics, Vol. 28, No. 3, May–June 2005.Presented as P...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2001.Includ...
As the demand for Unmanned Aerial System (UAS) technology increases, the current guidance, navigatio...
Copyright © 2002 by the author(s). Published by the American Institute of Aeronautics and Astronauti...
The article of record as published may be located at http://dx.doi.org/10.2514/1.42056The paper pres...
With the increasing demand for unmanned aerial vehicles (UAVs) in both military and civilian applica...
The method of implementing an adaptive PID controller using a reference model of an unmanned aerial ...
In this paper we present a system for automatic control of a quadrocopter based on the adaptive cont...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
This paper presents an actuator dynamics augmentation of the classical Disturbance Observer Based Co...