This paper describes a nonlinear deterministic controller design for a helicopter with an underslung external load system. A robust control approach is considered for the control law development. The system is considered as a cascade connection of an uncertain nonlinear system. The controller is designed to ensure the stabilization of the helicopter system and the positioning of the underslung load at hover condition. Control analysis and numerical results show that the proposed controller is able to locate the load at the specified position or its neighbourhood
18th World CongressThe International Federation of Automatic ControlMilano (Italy) August 28 - Septe...
A control strategy for stabilization of single-point sling loads and hoists is proposed. Nonlinear ...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
The paper at hand addresses the positioning control of helicopter sling loads. Due to a significant ...
The paper at hand addresses the precise positioning control of helicopter sling loads. Due to a sign...
Controlling the position and attitude of a helicopter hovering in the presence of atmospheric turbul...
Abstract—We consider the problem of controlling the vertical motion of a nonlinear model of a helico...
In this work, a trajectory tracking controller structure for a systemcomposed of a load and an aeria...
This thesis addresses some of the issues associated with linear systems subject to nonlinearities at...
The paper illustrates a robust control scheme for application to helicopters in vertical flight mode...
Abstract: In this paper, a new anti-swing controller for helicopter slung load system near hover fli...
When a helicopter is required to hover with minimum deviations from a desired position without measu...
This article investigates modeling and modern control for a helicopter and slung-load system. For th...
This project aims at designing an on-line controller in the form of a Multi Input\ud Multi Output Se...
18th World CongressThe International Federation of Automatic ControlMilano (Italy) August 28 - Septe...
A control strategy for stabilization of single-point sling loads and hoists is proposed. Nonlinear ...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
The paper at hand addresses the positioning control of helicopter sling loads. Due to a significant ...
The paper at hand addresses the precise positioning control of helicopter sling loads. Due to a sign...
Controlling the position and attitude of a helicopter hovering in the presence of atmospheric turbul...
Abstract—We consider the problem of controlling the vertical motion of a nonlinear model of a helico...
In this work, a trajectory tracking controller structure for a systemcomposed of a load and an aeria...
This thesis addresses some of the issues associated with linear systems subject to nonlinearities at...
The paper illustrates a robust control scheme for application to helicopters in vertical flight mode...
Abstract: In this paper, a new anti-swing controller for helicopter slung load system near hover fli...
When a helicopter is required to hover with minimum deviations from a desired position without measu...
This article investigates modeling and modern control for a helicopter and slung-load system. For th...
This project aims at designing an on-line controller in the form of a Multi Input\ud Multi Output Se...
18th World CongressThe International Federation of Automatic ControlMilano (Italy) August 28 - Septe...
A control strategy for stabilization of single-point sling loads and hoists is proposed. Nonlinear ...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...