This article presents design and optimization results from an implementation of a novel disturbance decoupling control strategy for a small-scale unmanned helicopter. Such a strategy is based on the active disturbance rejection control (ADRC) method. It offers an appealing alternative to existing control approaches for helicopters by combining decoupling and disturbance rejection without a detailed plant dynamics. The tuning of the control system is formulated as a function optimization problem to capture various design considerations. In comparison with several different iterative search algorithms, an artificial bee colony (ABC) algorithm is selected to obtain the optimal control parameters. For a fair comparison of control performance, a...
\u3cp\u3eThis paper presents and compares approaches to the design of flight controllers for quadrot...
This thesis is concerned with robust control theory and its application to the autonomous flight con...
This thesis presents one of the first applications of H∞-optimization to the design of controllers f...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
Autonomous helicopter stabilization in the presence of a wind disturbance is presented. A controller...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The compound unmanned aircraft is provided with three primary flight modes, which are helicopter fli...
[[abstract]]This paper presents a synthesis of the decoupling compensator for multiinput multioutput...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
With the increased use of small unmanned systems, and even automated flight, safety is becoming an is...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
The task of control of unmanned helicopters is rather complicated in the presence of parametric unce...
Helicopters are complex, coupled dynamic systems with unstable behavior. Countless studies have show...
This article focuses on linear matrix inequality-based controller designs that can achieve stabiliza...
A new approach to optimal decoupling for multi-input multi-output (MIMO), linear, time-invariant con...
\u3cp\u3eThis paper presents and compares approaches to the design of flight controllers for quadrot...
This thesis is concerned with robust control theory and its application to the autonomous flight con...
This thesis presents one of the first applications of H∞-optimization to the design of controllers f...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
Autonomous helicopter stabilization in the presence of a wind disturbance is presented. A controller...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The compound unmanned aircraft is provided with three primary flight modes, which are helicopter fli...
[[abstract]]This paper presents a synthesis of the decoupling compensator for multiinput multioutput...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
With the increased use of small unmanned systems, and even automated flight, safety is becoming an is...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
The task of control of unmanned helicopters is rather complicated in the presence of parametric unce...
Helicopters are complex, coupled dynamic systems with unstable behavior. Countless studies have show...
This article focuses on linear matrix inequality-based controller designs that can achieve stabiliza...
A new approach to optimal decoupling for multi-input multi-output (MIMO), linear, time-invariant con...
\u3cp\u3eThis paper presents and compares approaches to the design of flight controllers for quadrot...
This thesis is concerned with robust control theory and its application to the autonomous flight con...
This thesis presents one of the first applications of H∞-optimization to the design of controllers f...